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Document 32016R1375
Commission Implementing Regulation (EU) 2016/1375 of 29 July 2016 amending Council Regulation (EU) No 267/2012 concerning restrictive measures against Iran
Commission Implementing Regulation (EU) 2016/1375 of 29 July 2016 amending Council Regulation (EU) No 267/2012 concerning restrictive measures against Iran
Commission Implementing Regulation (EU) 2016/1375 of 29 July 2016 amending Council Regulation (EU) No 267/2012 concerning restrictive measures against Iran
C/2016/5106
OJ L 221, 16.8.2016, p. 1–201
(BG, ES, CS, DA, DE, ET, EL, EN, FR, HR, IT, LV, LT, HU, MT, NL, PL, PT, RO, SK, SL, FI, SV)
In force
16.8.2016 |
EN |
Official Journal of the European Union |
L 221/1 |
COMMISSION IMPLEMENTING REGULATION (EU) 2016/1375
of 29 July 2016
amending Council Regulation (EU) No 267/2012 concerning restrictive measures against Iran
THE EUROPEAN COMMISSION,
Having regard to the Treaty on the Functioning of the European Union,
Having regard to Council Regulation (EU) No 267/2012 (1), and in particular Article 45 thereof,
Whereas:
(1) |
Regulation (EU) No 267/2012 gives effect to the measures provided for in Decision 2010/413/CFSP of 26 July 2010 concerning restrictive measures against Iran and repealing Common Position 2007/140/CFSP (2). |
(2) |
On 18 October 2015, the Council adopted Council Regulation (EU) 2015/1861 (3) amending Regulation (EU) No 267/2012. |
(3) |
Regulation (EU) 2015/1861 introduced Annexes I and III and amended Annex VIIB, among others. Annex I comprises the items, including goods, technology and software, contained in the Nuclear Suppliers Group (NSG) list. Annex III comprises items, including goods and technology, contained in the Missile Technology Control Regime (MTCR) list. Annex VIIB contains a list of graphite and raw or semi-finished metals. |
(4) |
Article 45 of Regulation (EU) No 267/2012 empowers the Commission to amend Annexes I, III and VIIB. Pursuant to this Article and in order to facilitate implementation, Annexes I and III should be supplemented with information allowing a better identification of the items in those Annexes by reference to existing identifying codes as applied under Annex I to Council Regulation (EC) No 428/2009 (4). Moreover, certain technical amendments should also be made to Annex VIIB, |
HAS ADOPTED THIS REGULATION:
Article 1
Regulation (EU) No 267/2012 is amended as follows:
(1) |
Annex I is replaced by Annex I to this Regulation; |
(2) |
Annex III is replaced by Annex II to this Regulation; |
(3) |
Annex VIIB is replaced by Annex III to this Regulation. |
Article 2
This Regulation shall enter into force on the day following that of its publication in the Official Journal of the European Union.
This Regulation shall be binding in its entirety and directly applicable in all Member States.
Done at Brussels, 29 July 2016.
For the Commission,
On behalf of the President,
Head of the Service for Foreign Policy Instruments
(1) Council Regulation (EU) No 267/2012 of 23 March 2012 concerning restrictive measures against Iran and repealing Regulation (EU) No 961/2010 (OJ L 88, 24.3.2012, p. 1).
(2) OJ L 195, 27.7.2010. p. 39.
(3) Council Regulation (EU) 2015/1861 of 18 October 2015 amending Regulation (EU) No 267/2012 concerning restrictive measures against Iran (OJ L 274, 18.10.2015, p. 1).
(4) Council Regulation (EC) No 428/2009 of 5 May 2009 setting up a Community regime for the control of exports, transfer, brokering and transit of dual-use items (OJ L 134, 29.5.2009, p. 1).
ANNEX I
‘ANNEX I
CATEGORY 0 — NUCLEAR MATERIALS, FACILITIES, AND EQUIPMENT
0A Systems, Equipment and Components
The corresponding systems, equipment and components as identified in Council Regulation (EC) No 428/2009 of 5 May 2009 setting up a Community regime for the control of exports, transfer, brokering and transit of dual-use items |
Nuclear Suppliers Group's control list as in INFCIRC/254/Rev.12/Part 1 (1) |
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0A001 |
“Nuclear reactors” and specially designed or prepared equipment and components therefor, as follows: |
TLB1.1 |
Complete nuclear reactors |
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0A001.a |
“Nuclear reactors”; |
TLB1.1 |
Nuclear reactors capable of operation so as to maintain a controlled self-sustaining fission chain reaction. EXPLANATORY NOTE A “nuclear reactor” basically includes the items within or attached directly to the reactor vessel, the equipment which controls the level of power in the core, and the components which normally contain or come in direct contact with or control the primary coolant of the reactor core. EXPORTS The export of the whole set of major items within this boundary will take place only in accordance with the procedures of the Guidelines. Those individual items within this functionally defined boundary which will be exported only in accordance with the procedures of the Guidelines are listed in paragraphs 1.2. to 1.11. The Government reserves to itself the right to apply the procedures of the Guidelines to other items within the functionally defined boundary |
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0A001.b |
Metal vessels, or major shop-fabricated parts therefor, including the reactor vessel head for a reactor pressure vessel, specially designed or prepared to contain the core of a “nuclear reactor”; |
TLB1.2 |
Nuclear reactor vessels Metal vessels, or major shop-fabricated parts therefor, especially designed or prepared to contain the core of a nuclear reactor as defined in paragraph 1.1. above, as well as relevant reactor internals as defined in paragraph 1.8. below. EXPLANATORY NOTE Item 1.2 covers nuclear reactor vessels regardless of pressure rating and includes reactor pressure vessels and calandrias. The reactor vessel head is covered by item 1.2. as a major shop-fabricated part of a reactor vessel. |
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0A001.c |
Manipulative equipment specially designed or prepared for inserting or removing fuel in a “nuclear reactor”; |
TLB1.3 |
Nuclear reactor fuel charging and discharging machines Manipulative equipment especially designed or prepared for inserting or removing fuel in a nuclear reactor as defined in paragraph 1.1. above. EXPLANATORY NOTE The items noted above are capable of on-load operation or at employing technically sophisticated positioning or alignment features to allow complex off-load fueling operations such as those in which direct viewing of or access to the fuel is not normally available. |
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0A001.d |
Control rods specially designed or prepared for the control of the fission process in a “nuclear reactor”, support or suspension structures therefor, rod drive mechanisms and rod guide tubes; |
TLB1.4 |
Nuclear reactor control rods and equipment Especially designed or prepared rods, support or suspension structures therefor, rod drive mechanisms or rod guide tubes to control the fission process in a nuclear reactor as defined in paragraph 1.1. above. |
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0A001.e |
Pressure tubes specially designed or prepared to contain both fuel elements and the primary coolant in a “nuclear reactor”; |
TLB1.5 |
Nuclear reactor pressure tubes Tubes which are especially designed or prepared to contain both fuel elements and the primary coolant in a reactor as defined in paragraph 1.1. above. EXPLANATORY NOTE Pressure tubes are parts of fuel channels designed to operate at elevated pressure, sometimes in excess of 5 MPa. |
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0A001.f |
Zirconium metal tubes or zirconium alloy tubes (or assembles of tubes) specially designed or prepared for use as fuel cladding in a “nuclear reactor”, and in quantities exceeding 10 kg;
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TLB1.6 |
Nuclear fuel cladding Zirconium metal tubes or zirconium alloy tubes (or assemblies of tubes) especially designed or prepared for use as fuel cladding in a reactor as defined in paragraph 1.1. above, and in quantities exceeding 10 kg.
EXPLANATORY NOTE Zirconium metal tubes or zirconium alloy tubes for use in a nuclear reactor consist of zirconium in which the relation of hafnium to zirconium is typically less than 1:500 parts by weight |
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0A001.g |
Coolant pumps or circulators specially designed or prepared for circulating the primary coolant of “nuclear reactors”; |
TLB1.7 |
Primary coolant pumps or circulators Pumps or circulators especially designed or prepared for circulating the primary coolant for nuclear reactors as defined in paragraph 1.1. above. EXPLANATORY NOTE: Especially designed or prepared pumps or circulators include pumps for water-cooled reactors, circulators for gas-cooled reactors, and electromagnetic and mechanical pumps for liquid-metal-cooled reactors. This equipment may include pumps with elaborate sealed or multi-sealed systems to prevent leakage of primary coolant, canned-driven pumps, and pumps with inertial mass systems. This definition encompasses pumps certified to Section III, Division I, Subsection NB (Class 1 components) of the American Society of Mechanical Engineers (ASME) Code, or equivalent standards. |
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0A001.h |
‘Nuclear reactor internals’ specially designed or prepared for use in a “nuclear reactor”, including support columns for the core, fuel channels, calandria tubes, thermal shields, baffles, core grid plates, and diffuser plates; Technical Note: In 0A001.h. ‘nuclear reactor internals’ means any major structure within a reactor vessel which has one or more functions such as supporting the core, maintaining fuel alignment, directing primary coolant flow, providing radiation shields for the reactor vessel, and guiding in-core instrumentation. |
TLB1.8 |
Nuclear reactor internals “Nuclear reactor internals” especially designed or prepared for use in a nuclear reactor as defined in paragraph 1.1 above. This includes, for example, support columns for the core, fuel channels, calandria tubes, thermal shields, baffles, core grid plates, and diffuser plates. EXPLANATORY NOTE “Nuclear reactor internals” are major structures within a reactor vessel which have one or more functions such as supporting the core, maintaining fuel alignment, directing primary coolant flow, providing radiation shields for the reactor vessel, and guiding in-core instrumentation. |
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0A001.i |
Heat exchangers as follows:
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TLB1.9 |
Heat exchangers (a) Steam generators especially designed or prepared for the primary, or intermediate, coolant circuit of a nuclear reactor as defined in paragraph 1.1 above. (b) Other heat exchangers especially designed or prepared for use in the primary coolant circuit of a nuclear reactor as defined in paragraph 1.1 above. EXPLANATORY NOTE Steam generators are especially designed or prepared to transfer the heat generated in the reactor to the feed water for steam generation. In the case of a fast reactor for which an intermediate coolant loop is also present, the steam generator is in the intermediate circuit. In a gas-cooled reactor, a heat exchanger may be utilized to transfer heat to a secondary gas loop that drives a gas turbine. The scope of control for this entry does not include heat exchangers for the supporting systems of the reactor, e.g., the emergency cooling system or the decay heat cooling system. |
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0A001.j |
Neutron detectors specially designed or prepared for determining neutron flux levels within the core of a “nuclear reactor”; |
TLB1.10 |
Neutron detectors Especially designed or prepared neutron detectors for determining neutron flux levels within the core of a reactor as defined in paragraph 1.1. above. EXPLANATORY NOTE The scope of this entry encompasses in-core and ex-core detectors which measure flux levels in a large range, typically from 104 neutrons per cm2 per second to 1010 neutrons per cm2 per second or more. Ex-core refers to those instruments outside the core of a reactor as defined in paragraph 1.1. above, but located within the biological shielding. |
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0A001.k |
‘External thermal shields’ specially designed or prepared for use in a “nuclear reactor” for the reduction of heat loss and also for the containment vessel protection. Technical Note: In 0A001.k. ‘external thermal shields’ means major structures placed over the reactor vessel which reduce heat loss from the reactor and reduce temperature within the containment vessel. |
TLB1.11 |
External thermal shields “External thermal shields” especially designed or prepared for use in a nuclear reactor as defined in paragraph 1.1 for reduction of heat loss and also for containment vessel protection. EXPLANATORY NOTE “External thermal shields” are major structures placed over the reactor vessel which reduce heat loss from the reactor and reduce temperature within the containment vessel. |
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0B001 |
Plant for the separation of isotopes of “natural uranium”, “depleted uranium” or “special fissile materials”, and specially designed or prepared equipment and components therefor, as follows: |
TLB5 |
Plants for the separation of isotopes of natural uranium, depleted uranium or special fissionable material and equipment, other than analytical instruments, especially designed or prepared therefor |
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0B001.a |
Plant specially designed for separating isotopes of “natural uranium”, “depleted uranium”, or “special fissile materials”, as follows:
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TLB5 |
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0B001.b |
Gas centrifuges and assemblies and components, specially designed or prepared for gas centrifuge separation process, as follows: Technical Note: In 0B001.b. ‘high strength-to-density ratio material’ means any of the following:
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TLB5.1 |
5.1. Gas centrifuges and assemblies and components especially designed or prepared for use in gas centrifuges INTRODUCTORY NOTE The gas centrifuge normally consists of a thin-walled cylinder(s) of between 75 mm and 650 mm diameter contained in a vacuum environment and spun at high peripheral speed of the order of 300 m/s or more with its central axis vertical. In order to achieve high speed the materials of construction for the rotating components have to be of a high strength to density ratio and the rotor assembly, and hence its individual components, have to be manufactured to very close tolerances in order to minimize the unbalance. In contrast to other centrifuges, the gas centrifuge for uranium enrichment is characterized by having within the rotor chamber a rotating disc-shaped baffle(s) and a stationary tube arrangement for feeding and extracting the UF6 gas and featuring at least three separate channels, of which two are connected to scoops extending from the rotor axis towards the periphery of the rotor chamber. Also contained within the vacuum environment are a number of critical items which do not rotate and which although they are especially designed are not difficult to fabricate nor are they fabricated out of unique materials. A centrifuge facility however requires a large number of these components, so that quantities can provide an important indication of end use. |
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0B001.b |
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TLB5.1.1 |
Rotating components |
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0B001.b. |
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TLB5.1.1a |
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0B001.b. |
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TLB5.1.1b |
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0B001.b. |
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TLB5.1.1c |
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0B001.b. |
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TLB5.1.1d |
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0B001.b. |
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TLB5.1.1e |
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TLB5.1.1 |
EXPLANATORY NOTE The materials used for centrifuge rotating components include the following:
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0B001.b |
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TLB5.1.2 |
Static components |
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0B001.b. |
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TLB5.1.2A.1 |
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0B001.b. |
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TLB5.1.2a2 |
EXPLANATORY NOTE These bearings usually have the following characteristics:
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0B001.b. |
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TLB5.1.2b |
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0B001.b. |
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TLB5.1.2c |
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0B001.b. |
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TLB5.1.2d |
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0B001.b. |
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TLB5.1.2e |
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0B001.b. |
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TLB5.1.2f |
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0B001.b. |
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TLB5.2.5 |
5.2.5. Frequency changers Frequency changers (also known as converters or inverters) especially designed or prepared to supply motor stators as defined under 5.1.2.(d), or parts, components and sub-assemblies of such frequency changers having all of the following characteristics:
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0B001.b. |
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TLB5.2.3 |
5.2.3 Special shut-off and control valves
EXPLANATORY NOTE Typical especially designed or prepared valves include bellow-sealed valves, fast acting closure-types, fast acting valves and others. |
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0B001.c |
Equipment and components, specially designed or prepared for gaseous diffusion separation process, as follows:
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TLB5.3.1a |
Gaseous diffusion barriers and barrier materials
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0B001.c |
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TLB5.3.2 |
Diffuser housings Especially designed or prepared hermetically sealed vessels for containing the gaseous diffusion barrier, made of or protected by UF6-resistant materials (see EXPLANATORY NOTE to section 5.4). |
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0B001.c |
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TLB5.3.3 |
Compressors and gas blowers Especially designed or prepared compressors or gas blowers with a suction volume capacity of 1 m3 per minute or more of UF6, and with a discharge pressure of up to 500 kPa, designed for long-term operation in the UF6 environment, as well as separate assemblies of such compressors and gas blowers. These compressors and gas blowers have a pressure ratio of 10:1 or less and are made of, or protected by, materials resistant to UF6 (see EXPLANATORY NOTE to section 5.4). |
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0B001.c |
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TLB5.3.4 |
Rotary shaft seals Especially designed or prepared vacuum seals, with seal feed and seal exhaust connections, for sealing the shaft connecting the compressor or the gas blower rotor with the driver motor so as to ensure a reliable seal against in-leaking of air into the inner chamber of the compressor or gas blower which is filled with UF6. Such seals are normally designed for a buffer gas in-leakage rate of less than 1 000 cm3 per minute. |
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0B001.c |
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TLB5.3.5 |
Heat exchangers for cooling UF6 Especially designed or prepared heat exchangers made of or protected by UF6-resistant materials (see EXPLANATORY NOTE to section 5.4), and intended for a leakage pressure change rate of less than 10 Pa per hour under a pressure difference of 100 kPa. |
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0B001.c |
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TLB5.4.4 |
Special shut-off and control valves Especially designed or prepared bellows-sealed valves, manual or automated, shut-off or control, made of or protected by materials resistant to corrosion by UF6, for installation in main and auxiliary systems of gaseous diffusion enrichment plants. |
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0B001.d |
Equipment and components, specially designed or prepared for aerodynamic separation process, as follows:
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TLB5.5.1 |
Separation nozzles Especially designed or prepared separation nozzles and assemblies thereof. The separation nozzles consist of slit-shaped, curved channels having a radius of curvature less than 1 mm, resistant to corrosion by UF6 and having a knife-edge within the nozzle that separates the gas flowing through the nozzle into two fractions. |
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0B001.d |
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TLB5.5.2 |
Vortex tubes Especially designed or prepared vortex tubes and assemblies thereof. The vortex tubes are cylindrical or tapered, made of or protected by materials resistant to corrosion by UF6, and with one or more tangential inlets. The tubes may be equipped with nozzletype appendages at either or both ends. EXPLANATORY NOTE The feed gas enters the vortex tube tangentially at one end or through swirl vanes or at numerous tangential positions along the periphery of the tube. |
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0B001.d |
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TLB5.5.3 TLB5.5.4 |
Compressors and gas blowers Especially designed or prepared compressors or gas blowers made of or protected by materials resistant to corrosion by the UF6/carrier gas (hydrogen or helium) mixture. Rotary shaft seals Especially designed or prepared rotary shaft seals, with seal feed and seal exhaust connections, for sealing the shaft connecting the compressor rotor or the gas blower rotor with the driver motor so as to ensure a reliable seal against out-leakage of process gas or in-leakage of air or seal gas into the inner chamber of the compressor or gas blower which is filled with a UF6/carrier gas mixture. |
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0B001.d |
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TLB5.5.5 |
Heat exchangers for gas cooling Especially designed or prepared heat exchangers made of or protected by materials resistant to corrosion by UF6. |
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0B001.d |
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TLB5.5.6 |
Separation element housings Especially designed or prepared separation element housings, made of or protected by materials resistant to corrosion by UF6, for containing vortex tubes or separation nozzles. |
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0B001.d |
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TLB5.5.10 |
UF6 mass spectrometers/Ion sources Especially designed or prepared mass spectrometers capable of taking on-line samples from UF6 gas streams and having all of the following:
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0B001.d |
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TLB5.5.12 |
UF6/carrier gas separation systems Especially designed or prepared process systems for separating UF6 from carrier gas (hydrogen or helium). EXPLANATORY NOTE These systems are designed to reduce the UF6 content in the carrier gas to 1 ppm or less and may incorporate equipment such as:
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0B001.e |
Equipment and components, specially designed or prepared for chemical exchange separation process, as follows:
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TLB5.6.1 |
Liquid-liquid exchange columns (Chemical exchange) Countercurrent liquid-liquid exchange columns having mechanical power input, especially designed or prepared for uranium enrichment using the chemical exchange process. For corrosion resistance to concentrated hydrochloric acid solutions, these columns and their internals are normally made of or protected by suitable plastic materials (such as fluorinated hydrocarbon polymers) or glass. The stage residence time of the columns is normally designed to be 30 seconds or less. |
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0B001.e |
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TLB5.6.2 |
Liquid-liquid centrifugal contactors (Chemical exchange) Liquid-liquid centrifugal contactors especially designed or prepared for uranium enrichment using the chemical exchange process. Such contactors use rotation to achieve dispersion of the organic and aqueous streams and then centrifugal force to separate the phases. For corrosion resistance to concentrated hydrochloric acid solutions, the contactors are normally made of or protected by suitable plastic materials (such as fluorinated hydrocarbon polymers) or glass. The stage residence time of the centrifugal contactors is normally designed to be 30 seconds or less. |
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0B001.e |
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TLB5.6.3a |
Uranium reduction systems and equipment (Chemical exchange)
EXPLANATORY NOTE The cell cathodic compartment must be designed to prevent re-oxidation of uranium to its higher valence state. To keep the uranium in the cathodic compartment, the cell may have an impervious diaphragm membrane constructed of special cation exchange material. The cathode consists of a suitable solid conductor such as graphite. |
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0B001.e |
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TLB5.6.3b |
EXPLANATORY NOTE These systems consist of solvent extraction equipment for stripping the U+4 from the organic stream into an aqueous solution, evaporation and/or other equipment to accomplish solution pH adjustment and control, and pumps or other transfer devices for feeding to the electrochemical reduction cells. A major design concern is to avoid contamination of the aqueous stream with certain metal ions. Consequently, for those parts in contact with the process stream, the system is constructed of equipment made of or protected by suitable materials (such as glass, fluorocarbon polymers, polyphenyl sulfate, polyether sulfone, and resinimpregnated graphite). |
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0B001.e |
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TLB5.6.4 |
Feed preparation systems (Chemical exchange) Especially designed or prepared systems for producing high-purity uranium chloride feed solutions for chemical exchange uranium isotope separation plants. EXPLANATORY NOTE These systems consist of dissolution, solvent extraction and/or ion exchange equipment for purification and electrolytic cells for reducing the uranium U+6 or U+4 to U+3. These systems produce uranium chloride solutions having only a few parts per million of metallic impurities such as chromium, iron, vanadium, molybdenum and other bivalent or higher multi-valent cations. Materials of construction for portions of the system processing high-purity U+3 include glass, fluorinated hydrocarbon polymers, polyphenyl sulfate or polyether sulfone plastic-lined and resin-impregnated graphite. NSG Part 1 June 2013 - 39 - 5.6.5. Uranium |
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0B001.e |
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TLB5.6.5 |
Uranium oxidation systems (Chemical exchange) Especially designed or prepared systems for oxidation of U+3 to U+4 for return to the uranium isotope separation cascade in the chemical exchange enrichment process. EXPLANATORY NOTE These systems may incorporate equipment such as: (a) Equipment for contacting chlorine and oxygen with the aqueous effluent from the isotope separation equipment and extracting the resultant U+4 into the stripped organic stream returning from the product end of the cascade, (b) Equipment that separates water from hydrochloric acid so that the water and the concentrated hydrochloric acid may be reintroduced to the process at the proper locations. |
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0B001.f |
Equipment and components, specially designed or prepared for ion-exchange separation process, as follows:
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TLB5.6.6 |
Fast-reacting ion exchange resins/adsorbents (Ion exchange) Fast-reacting ion-exchange resins or adsorbents especially designed or prepared for uranium enrichment using the ion exchange process, including porous macroreticular resins, and/or pellicular structures in which the active chemical exchange groups are limited to a coating on the surface of an inactive porous support structure, and other composite structures in any suitable form including particles or fibres. These ion exchange resins/adsorbents have diameters of 0,2 mm or less and must be chemically resistant to concentrated hydrochloric acid solutions as well as physically strong enough so as not to degrade in the exchange columns. The resins/adsorbents are especially designed to achieve very fast uranium isotope exchange kinetics (exchange rate half-time of less than 10 seconds) and are capable of operating at a temperature in the range of 373 K (100 °C) to 473 K (200 °C). |
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0B001.f |
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TLB5.6.7 |
Ion exchange columns (Ion exchange) Cylindrical columns greater than 1 000 mm in diameter for containing and supporting packed beds of ion exchange resin/adsorbent, especially designed or prepared for uranium enrichment using the ion exchange process. These columns are made of or protected by materials (such as titanium or fluorocarbon plastics) resistant to corrosion by concentrated hydrochloric acid solutions and are capable of operating at a temperature in the range of 373 K (100 °C) to 473 K (200 °C) and pressures above 0,7 MPa. |
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0B001.f |
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TLB5.6.8 |
Ion exchange reflux systems (Ion exchange) (a) Especially designed or prepared chemical or electrochemical reduction systems for regeneration of the chemical reducing agent(s) used in ion exchange uranium enrichment cascades. (b) Especially designed or prepared chemical or electrochemical oxidation systems for regeneration of the chemical oxidizing agent(s) used in ion exchange uranium enrichment cascades. |
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0B001.g |
Equipment and components, specially designed or prepared for laser-based separation processes using atomic vapour laser isotope separation, as follows:
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TLB5.7.1 |
Uranium vaporization systems (atomic vapour based methods) Especially designed or prepared uranium metal vaporization systems for use in laser enrichment. EXPLANATORY NOTE These systems may contain electron beam guns and are designed to achieve a delivered power (1 kW or greater) on the target sufficient to generate uranium metal vapour at a rate required for the laser enrichment function. |
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0B001.g |
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TLB5.7.2 |
Liquid or vapour uranium metal handling systems and components (atomic vapour based methods) Especially designed or prepared systems for handling molten uranium, molten uranium alloys or uranium metal vapour for use in laser enrichment or especially designed or prepared components therefore. EXPLANATORY NOTE The liquid uranium metal handling systems may consist of crucibles and cooling equipment for the crucibles. The crucibles and other parts of this system that come into contact with molten uranium, molten uranium alloys or uranium metal vapour are made of or protected by materials of suitable corrosion and heat resistance. Suitable materials may include tantalum, yttria-coated graphite, graphite coated with other rare earth oxides (see INFCIRC/254/Part 2 — (as amended)) or mixtures thereof. |
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0B001.g |
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TLB5.7.3 |
Uranium metal ‘product’ and ‘tails’ collector assemblies (atomic vapour based methods) Especially designed or prepared ‘product’ and ‘tails’ collector assemblies for uranium metal in liquid or solid form. EXPLANATORY NOTE Components for these assemblies are made of or protected by materials resistant to the heat and corrosion of uranium metal vapour or liquid (such as yttria-coated graphite or tantalum) and may include pipes, valves, fittings, ‘gutters’, feed-throughs, heat exchangers and collector plates for magnetic, electrostatic or other separation methods. |
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0B001.g |
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TLB5.7.4 |
Separator module housings (atomic vapour based methods) Especially designed or prepared cylindrical or rectangular vessels for containing the uranium metal vapour source, the electron beam gun, and the ‘product’ and ‘tails’ collectors. EXPLANATORY NOTE These housings have multiplicity of ports for electrical and water feed-throughs, laser beam windows, vacuum pump connections and instrumentation diagnostics and monitoring. They have provisions for opening and closure to allow refurbishment of internal components. |
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0B001.g |
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TLB5.7.13 |
Laser systems Lasers or laser systems especially designed or prepared for the separation of uranium isotopes. EXPLANATORY NOTE The lasers and laser components of importance in laser-based enrichment processes include those identified in INFCIRC/254/Part 2 — (as amended). The laser system typically contains both optical and electronic components for the management of the laser beam (or beams) and the transmission to the isotope separation chamber. The laser system for atomic vapour based methods usually consists of tunable dye lasers pumped by another type of laser (e.g., copper vapour lasers or certain solid-state lasers). The laser system for molecular based methods may consist of CO2 lasers or excimer lasers and a multi-pass optical cell. Lasers or laser systems for both methods require spectrum frequency stabilization for operation over extended periods of time. |
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0B001.h |
Equipment and components, specially designed or prepared for laser-based separation processes using molecular laser isotope separation, as follows:
|
TLB5.7.5 |
Supersonic expansion nozzles (molecular based methods) Especially designed or prepared supersonic expansion nozzles for cooling mixtures of UF6 and carrier gas to 150 K (–123 °C) or less and which are corrosion resistant to UF6. |
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0B001.h |
|
TLB5.7.6 |
‘Product’ or ‘tails’ collectors (molecular based methods) Especially designed or prepared components or devices for collecting uranium product material or uranium tails material following illumination with laser light. EXPLANATORY NOTE In one example of molecular laser isotope separation, the product collectors serve to collect enriched uranium pentafluoride (UF5) solid material. The product collectors may consist of filter, impact, or cyclone-type collectors, or combinations thereof, and must be corrosion resistant to the UF5/ UF6 environment. |
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0B001.h |
|
TLB5.7.7 |
UF6/carrier gas compressors (molecular based methods) Especially designed or prepared compressors for UF6/carrier gas mixtures, designed for long term operation in a UF6 environment. The components of these compressors that come into contact with process gas are made of or protected by materials resistant to corrosion by UF6. |
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TLB5.7.8 |
Rotary shaft seals (molecular based methods) Especially designed or prepared rotary shaft seals, with seal feed and seal exhaust connections, for sealing the shaft connecting the compressor rotor with the driver motor so as to ensure a reliable seal against out-leakage of process gas or in-leakage of air or seal gas into the inner chamber of the compressor which is filled with a UF6/carrier gas mixture. |
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0B001.h |
|
TLB5.7.9 |
Fluorination systems (molecular based methods) Especially designed or prepared systems for fluorinating UF5 (solid) to UF6 (gas). EXPLANATORY NOTE These systems are designed to fluorinate the collected UF5 powder to UF6 for subsequent collection in product containers or for transfer as feed for additional enrichment. In one approach, the fluorination reaction may be accomplished within the isotope separation system to react and recover directly off the ‘product’ collectors. In another approach, the UF5 powder may be removed/transferred from the ‘product’ collectors into a suitable reaction vessel (e.g., fluidized-bed reactor, screw reactor or flame tower) for fluorination. In both approaches, equipment for storage and transfer of fluorine (or other suitable fluorinating agents) and for collection and transfer of UF6 are used. |
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0B001.h |
|
TLB5.7.12 |
UF6/carrier gas separation systems (molecular based methods) Especially designed or prepared process systems for separating UF6 from carrier gas. EXPLANATORY NOTE These systems may incorporate equipment such as: (a) Cryogenic heat exchangers or cryoseparators capable of temperatures of 153 K (– 120 °C) or less, or (b) Cryogenic refrigeration units capable of temperatures of 153 K (–120 °C) or less, or (c) UF6 cold traps capable of freezing out UF6. The carrier gas may be nitrogen, argon, or other gas. |
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0B001.h |
|
TLB5.7.13 |
Laser systems Lasers or laser systems especially designed or prepared for the separation of uranium isotopes. EXPLANATORY NOTE The lasers and laser components of importance in laser-based enrichment processes include those identified in INFCIRC/254/Part 2 — (as amended). The laser system typically contains both optical and electronic components for the management of the laser beam (or beams) and the transmission to the isotope separation chamber. The laser system for atomic vapour based methods usually consists of tunable dye lasers pumped by another type of laser (e.g., copper vapour lasers or certain solid-state lasers). The laser system for molecular based methods may consist of CO2 lasers or excimer lasers and a multi-pass optical cell. Lasers or laser systems for both methods require spectrum frequency stabilization for operation over extended periods of time. |
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0B001.i |
Equipment and components, specially designed or prepared for plasma separation process, as follows:
|
TLB5.8.1 |
Microwave power sources and antennae Especially designed or prepared microwave power sources and antennae for producing or accelerating ions and having the following characteristics: greater than 30 GHz frequency and greater than 50 kW mean power output for ion production. |
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0B001.i |
|
TLB5.8.2 |
Ion excitation coils Especially designed or prepared radio frequency ion excitation coils for frequencies of more than 100 kHz and capable of handling more than 40 kW mean power. |
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0B001.i |
|
TLB5.8.3 |
Uranium plasma generation systems Especially designed or prepared systems for the generation of uranium plasma for use in plasma separation plants. |
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0B001.i |
|
TLB5.8.4 |
No longer used — since 14 June 2013 |
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0B001.i |
|
TLB5.8.5 |
Uranium metal ‘product’ and ‘tails’ collector assemblies Especially designed or prepared ‘product’ and ‘tails’ collector assemblies for uranium metal in solid form. These collector assemblies are made of or protected by materials resistant to the heat and corrosion of uranium metal vapor, such as yttria-coated graphite or tantalum. |
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0B001.i |
|
TLB.5.8.6 |
Separator module housings Cylindrical vessels especially designed or prepared for use in plasma separation enrichment plants for containing the uranium plasma source, radio-frequency drive coil and the “product” and “tails” collectors. EXPLANATORY NOTE These housings have a multiplicity of ports for electrical feed-throughs, diffusion pump connections and instrumentation diagnostics and monitoring. They have provisions for opening and closure to allow for refurbishment of internal components and are constructed of a suitable non-magnetic material such as stainless steel. |
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0B001.j |
Equipment and components, specially designed or prepared for electromagnetic separation process, as follows:
|
TLB5.9.1a |
Electromagnetic isotope separators Electromagnetic isotope separators especially designed or prepared for the separation of uranium isotopes, and equipment and components therefor, including:
|
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0B001.j |
|
TLB5.9.1b |
Ion collectors Collector plates consisting of two or more slits and pockets especially designed or prepared for collection of enriched and depleted uranium ion beams and constructed of suitable materials such as graphite or stainless steel. |
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0B001.j |
|
TLB5.9.1c |
Vacuum housings Especially designed or prepared vacuum housings for uranium electromagnetic separators, constructed of suitable non-magnetic materials such as stainless steel and designed for operation at pressures of 0,1 Pa or lower. EXPLANATORY NOTE The housings are specially designed to contain the ion sources, collector plates and water-cooled liners and have provision for diffusion pump connections and opening and closure for removal and reinstallation of these components. |
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0B001.j |
|
TLB5.9.1d |
Magnet pole pieces Especially designed or prepared magnet pole pieces having a diameter greater than 2 m used to maintain a constant magnetic field within an electromagnetic isotope separator and to transfer the magnetic field between adjoining separators. |
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0B001.j |
|
TLB5.9.2 |
High voltage power supplies Especially designed or prepared high-voltage power supplies for ion sources, having all of the following characteristics: capable of continuous operation, output voltage of 20 000 V or greater, output current of 1 A or greater, and voltage regulation of better than 0,01 % over a time period of 8 hours. |
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0B001.j |
|
TLB5.9.3 |
Magnet power supplies Especially designed or prepared high-power, direct current magnet power supplies having all of the following characteristics: capable of continuously producing a current output of 500 A or greater at a voltage of 100 V or greater and with a current or voltage regulation better than 0,01 % over a period of 8 hours. |
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0B002 |
Specially designed or prepared auxiliary systems, equipment and components, as follows, for isotope separation plant specified in 0B001, made of or protected by “materials resistant to corrosion by UF6”: |
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|
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0B002.a |
Feed autoclaves, ovens or systems used for passing UF6 to the enrichment process; |
TLB5.2.1 |
Feed systems/product and tails withdrawal systems Especially designed or prepared process systems or equipment for enrichment plants made of or protected by materials resistant to corrosion by UF6, including: (a) Feed autoclaves, ovens, or systems used for passing UF6 to the enrichment process; (b) Desublimers, cold traps or pumps used to remove UF6 from the enrichment process for subsequent transfer upon heating; (c) Solidification or liquefaction stations used to remove UF6 from the enrichment process by compressing and converting UF6 to a liquid or solid form; (d) ‘Product’ or ‘tails’ stations used for transferring UF6 into containers. |
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TLB5.4.1 |
Feed systems/product and tails withdrawal systems Especially designed or prepared process systems or equipment for enrichment plants made of or protected by materials resistant to corrosion by UF6, including: (a) Feed autoclaves, ovens, or systems used for passing UF6 to the enrichment process; (b) Desublimers, cold traps or pumps used to remove UF6 from the enrichment process for subsequent transfer upon heating; (c) Solidification or liquefaction stations used to remove UF6 from the enrichment process by compressing and converting UF6 to a liquid or solid form; (d) ‘Product’ or ‘tails’ stations used for transferring UF6 into containers. |
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TLB5.5.7 |
Feed systems/product and tails withdrawal systems Especially designed or prepared process systems or equipment for enrichment plants made of or protected by materials resistant to corrosion by UF6, including: (a) Feed autoclaves, ovens, or systems used for passing UF6 to the enrichment process; (b) Desublimers (or cold traps) used to remove UF6 from the enrichment process for subsequent transfer upon heating; (c) Solidification or liquefaction stations used to remove UF6 from the enrichment process by compressing and converting UF6 to a liquid or solid form; (d) ‘Product’ or ‘tails’ stations used for transferring UF6 into containers |
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TLB5.7.11 |
Feed systems/product and tails withdrawal systems (molecular based methods) Especially designed or prepared process systems or equipment for enrichment plants made of or protected by materials resistant to corrosion by UF6, including: (a) Feed autoclaves, ovens, or systems used for passing UF6 to the enrichment process; (b) Desublimers (or cold traps) used to remove UF6 from the enrichment process for subsequent transfer upon heating; (c) Solidification or liquefaction stations used to remove UF6 from the enrichment process by compressing and converting UF6 to a liquid or solid form; (d) ‘Product’ or ‘tails’ stations used for transferring UF6 into containers. |
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0B002.b |
Desublimers or cold traps, used to remove UF6 from the enrichment process for subsequent transfer upon heating; |
TLB5.2.1 |
Feed systems/product and tails withdrawal systems Especially designed or prepared process systems or equipment for enrichment plants made of or protected by materials resistant to corrosion by UF6, including: (a) Feed autoclaves, ovens, or systems used for passing UF6 to the enrichment process; (b) Desublimers, cold traps or pumps used to remove UF6 from the enrichment process for subsequent transfer upon heating; (c) Solidification or liquefaction stations used to remove UF6 from the enrichment process by compressing and converting UF6 to a liquid or solid form; (d) ‘Product’ or ‘tails’ stations used for transferring UF6 into containers. |
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TLB5.4.1 |
Feed systems/product and tails withdrawal systems Especially designed or prepared process systems or equipment for enrichment plants made of or protected by materials resistant to corrosion by UF6, including: (a) Feed autoclaves, ovens, or systems used for passing UF6 to the enrichment process; (b) Desublimers, cold traps or pumps used to remove UF6 from the enrichment process for subsequent transfer upon heating; (c) Solidification or liquefaction stations used to remove UF6 from the enrichment process by compressing and converting UF6 to a liquid or solid form; (d) ‘Product’ or ‘tails’ stations used for transferring UF6 into containers. |
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TLB5.5.7 |
Feed systems/product and tails withdrawal systems Especially designed or prepared process systems or equipment for enrichment plants made of or protected by materials resistant to corrosion by UF6, including: (a) Feed autoclaves, ovens, or systems used for passing UF6 to the enrichment process; (b) Desublimers (or cold traps) used to remove UF6 from the enrichment process for subsequent transfer upon heating; (c) Solidification or liquefaction stations used to remove UF6 from the enrichment process by compressing and converting UF6 to a liquid or solid form; (d) ‘Product’ or ‘tails’ stations used for transferring UF6 into containers. |
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TLB5.7.11 |
Feed systems/product and tails withdrawal systems (molecular based methods) Especially designed or prepared process systems or equipment for enrichment plants made of or protected by materials resistant to corrosion by UF6, including: (a) Feed autoclaves, ovens, or systems used for passing UF6 to the enrichment process; (b) Desublimers (or cold traps) used to remove UF6 from the enrichment process for subsequent transfer upon heating; (c) Solidification or liquefaction stations used to remove UF6 from the enrichment process by compressing and converting UF6 to a liquid or solid form; (d) ‘Product’ or ‘tails’ stations used for transferring UF6 into containers. |
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0B002.c |
Product and tails stations for transferring UF6 into containers; |
TLB5.2.1 |
Feed systems/product and tails withdrawal systems Especially designed or prepared process systems or equipment for enrichment plants made of or protected by materials resistant to corrosion by UF6, including: (a) Feed autoclaves, ovens, or systems used for passing UF6 to the enrichment process; (b) Desublimers, cold traps or pumps used to remove UF6 from the enrichment process for subsequent transfer upon heating; (c) Solidification or liquefaction stations used to remove UF6 from the enrichment process by compressing and converting UF6 to a liquid or solid form; (d) ‘Product’ or ‘tails’ stations used for transferring UF6 into containers. |
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TLB5.4.1 |
Feed systems/product and tails withdrawal systems Especially designed or prepared process systems or equipment for enrichment plants made of or protected by materials resistant to corrosion by UF6, including: (a) Feed autoclaves, ovens, or systems used for passing UF6 to the enrichment process; (b) Desublimers, cold traps or pumps used to remove UF6 from the enrichment process for subsequent transfer upon heating; (c) Solidification or liquefaction stations used to remove UF6 from the enrichment process by compressing and converting UF6 to a liquid or solid form; (d) ‘Product’ or ‘tails’ stations used for transferring UF6 into containers. |
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TLB5.5.7 |
Feed systems/product and tails withdrawal systems Especially designed or prepared process systems or equipment for enrichment plants made of or protected by materials resistant to corrosion by UF6, including: (a) Feed autoclaves, ovens, or systems used for passing UF6 to the enrichment process; (b) Desublimers (or cold traps) used to remove UF6 from the enrichment process for subsequent transfer upon heating; (c) Solidification or liquefaction stations used to remove UF6 from the enrichment process by compressing and converting UF6 to a liquid or solid form; (d) ‘Product’ or ‘tails’ stations used for transferring UF6 into containers. |
|||||||||||||||||||||
TLB5.7.11 |
Feed systems/product and tails withdrawal systems (molecular based methods) Especially designed or prepared process systems or equipment for enrichment plants made of or protected by materials resistant to corrosion by UF6, including: (a) Feed autoclaves, ovens, or systems used for passing UF6 to the enrichment process; (b) Desublimers (or cold traps) used to remove UF6 from the enrichment process for subsequent transfer upon heating; (c) Solidification or liquefaction stations used to remove UF6 from the enrichment process by compressing and converting UF6 to a liquid or solid form; (d) ‘Product’ or ‘tails’ stations used for transferring UF6 into containers. |
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0B002.d |
Liquefaction or solidification stations used to remove UF6 from the enrichment process by compressing, cooling and converting UF6 to a liquid or solid form; |
TLB5.2.1 |
Feed systems/product and tails withdrawal systems Especially designed or prepared process systems or equipment for enrichment plants made of or protected by materials resistant to corrosion by UF6, including: (a) Feed autoclaves, ovens, or systems used for passing UF6 to the enrichment process; (b) Desublimers, cold traps or pumps used to remove UF6 from the enrichment process for subsequent transfer upon heating; (c) Solidification or liquefaction stations used to remove UF6 from the enrichment process by compressing and converting UF6 to a liquid or solid form; (d) ‘Product’ or ‘tails’ stations used for transferring UF6 into containers. |
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TLB5.4.1 |
Feed systems/product and tails withdrawal systems Especially designed or prepared process systems or equipment for enrichment plants made of or protected by materials resistant to corrosion by UF6, including: (a) Feed autoclaves, ovens, or systems used for passing UF6 to the enrichment process; (b) Desublimers, cold traps or pumps used to remove UF6 from the enrichment process for subsequent transfer upon heating; (c) Solidification or liquefaction stations used to remove UF6 from the enrichment process by compressing and converting UF6 to a liquid or solid form; (d) ‘Product’ or ‘tails’ stations used for transferring UF6 into containers. |
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TLB5.5.7 |
Feed systems/product and tails withdrawal systems Especially designed or prepared process systems or equipment for enrichment plants made of or protected by materials resistant to corrosion by UF6, including: (a) Feed autoclaves, ovens, or systems used for passing UF6 to the enrichment process; (b) Desublimers (or cold traps) used to remove UF6 from the enrichment process for subsequent transfer upon heating; (c) Solidification or liquefaction stations used to remove UF6 from the enrichment process by compressing and converting UF6 to a liquid or solid form; (d) ‘Product’ or ‘tails’ stations used for transferring UF6 into containers. |
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TLB5.7.11 |
Feed systems/product and tails withdrawal systems (molecular based methods) Especially designed or prepared process systems or equipment for enrichment plants made of or protected by materials resistant to corrosion by UF6, including: (a) Feed autoclaves, ovens, or systems used for passing UF6 to the enrichment process; (b) Desublimers (or cold traps) used to remove UF6 from the enrichment process for subsequent transfer upon heating; (c) Solidification or liquefaction stations used to remove UF6 from the enrichment process by compressing and converting UF6 to a liquid or solid form; (d) ‘Product’ or ‘tails’ stations used for transferring UF6 into containers. |
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0B002.e |
Piping systems and header systems specially designed or prepared for handling UF6 within gaseous diffusion, centrifuge or aerodynamic cascades; |
TLB5.2.2 |
Machine header piping systems Especially designed or prepared piping systems and header systems for handling UF6 within the centrifuge cascades. The piping network is normally of the ‘triple’ header system with each centrifuge connected to each of the headers. There is thus a substantial amount of repetition in its form. It is wholly made of or protected by UF6-resistant materials (see EXPLANATORY NOTE to this section) and is fabricated to very high vacuum and cleanliness standards. |
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TLB5.4.2 |
Header piping systems Especially designed or prepared piping systems and header systems for handling UF6 within the gaseous diffusion cascades. EXPLANATORY NOTE This piping network is normally of the “double” header system with each cell connected to each of the headers. |
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TLB5.5.8 |
Header piping systems Especially designed or prepared header piping systems, made of or protected by materials resistant to corrosion by UF6, for handling UF6 within the aerodynamic cascades. This piping network is normally of the ‘double’ header design with each stage or group of stages connected to each of the headers. |
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0B002.f |
Vacuum systems and pumps as follows:
|
TLB5.4.3a |
Vacuum systems
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TLB5.4.3b |
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TLB5.5.9b |
Vacuum systems and pumps Vacuum pumps especially designed or prepared for service in UF6-bearing atmospheres and made of or protected by materials resistant to corrosion by UF6. These pumps may use fluorocarbon seals and special working fluids. |
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TLB5.5.9a |
Especially designed or prepared vacuum systems consisting of vacuum manifolds, vacuum headers and vacuum pumps, and designed for service in UF6-bearing atmospheres |
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0B002.g |
UF6 mass spectrometers/ion sources capable of taking on-line samples from UF6 gas streams and having all of the following:
|
TLB5.2.4 |
UF6 mass spectrometers/ion sources Especially designed or prepared mass spectrometers capable of taking on-line samples from UF6 gas streams and having all of the following:
|
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TLB5.4.5 |
UF6 mass spectrometers/ion sources Especially designed or prepared mass spectrometers capable of taking on-line samples from UF6 gas streams and having all of the following:
|
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TLB5.5.11 |
UF6 mass spectrometers/Ion sources Especially designed or prepared mass spectrometers capable of taking on-line samples from UF6 gas streams and having all of the following:
|
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TLB5.7.10 |
Special shut-off and control valves Especially designed or prepared bellows-sealed valves, manual or automated, shut-off or control, made of or protected by materials resistant to corrosion by UF6, with a diameter of 40 mm or greater, for installation in main and auxiliary systems of aerodynamic enrichment plants. |
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0B003 |
Plant for the conversion of uranium and equipment specially designed or prepared therefor, as follows: |
TLB7.1 |
Especially designed or prepared systems for the conversion of uranium ore concentrates to UO3 |
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0B003.a |
Systems for the conversion of uranium ore concentrates to UO3; |
TLB7.1.1 |
EXPLANATORY NOTE Conversion of uranium ore concentrates to UO3 can be performed by first dissolving the ore in nitric acid and extracting purified uranyl nitrate using a solvent such as tributyl phosphate. Next, the uranyl nitrate is converted to UO3 either by concentration and denitration or by neutralization with gaseous ammonia to produce ammonium diuranate with subsequent filtering, drying, and calcining |
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0B003.b |
Systems for the conversion of UO3 to UF6; |
TLB7.1.2 |
Especially designed or prepared systems for the conversion of UO3 to UF6 EXPLANATORY NOTE EXPLANATORY NOTE Conversion of UO3 to UO2 can be performed through reduction of UO3 with cracked ammonia gas or hydrogen. |
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0B003.c |
Systems for the conversion of UO3 to UO2; |
TLB7.1.3 |
Especially designed or prepared systems for the conversion of UO3 to UO2 EXPLANATORY NOTE Conversion of UO3 to UO2 can be performed through reduction of UO3 with cracked ammonia gas or hydrogen. |
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0B003.d |
Systems for the conversion of UO2 to UF4; |
TLB7.1.4 |
Especially designed or prepared systems for the conversion of UO2 to UF4 EXPLANATORY NOTE Conversion of UO2 to UF4 can be performed by reacting UO2 with hydrogen fluoride gas (HF) at 300-500 °C. |
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0B003.e |
Systems for the conversion of UF4 to UF6; |
TLB7.1.5 |
Especially designed or prepared systems for the conversion of UF4 to UF6 EXPLANATORY NOTE Conversion of UF4 to UF6 is performed by exothermic reaction with fluorine in a tower reactor. UF6 is condensed from the hot effluent gases by passing the effluent stream through a cold trap cooled to –10 °C. The process requires a source of fluorine gas |
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0B003.f |
Systems for the conversion of UF4 to uranium metal; |
TLB7.1.6 |
Especially designed or prepared systems for the conversion of UF4 to U metal EXPLANATORY NOTE Conversion of UF4 to U metal is performed by reduction with magnesium (large batches) or calcium (small batches). The reaction is carried out at temperatures above the melting point of uranium (1 130 °C). |
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0B003.g |
Systems for the conversion of UF6 to UO2; |
TLB7.1.7 |
Especially designed or prepared systems for the conversion of UF6 to UO2 EXPLANATORY NOTE Conversion of UF6 to UO2 can be performed by one of three processes. In the first, UF6 is reduced and hydrolyzed to UO2 using hydrogen and steam. In the second, UF6 is hydrolyzed by solution in water, ammonia is added to precipitate ammonium diuranate, and the diuranate is reduced to UO2 with hydrogen at 820 °C. In the third process, gaseous UF6, CO2, and NH3 are combined in water, precipitating ammonium uranyl carbonate. The ammonium uranyl carbonate is combined with steam and hydrogen at 500-600 °C to yield UO2. UF6 to UO2 conversion is often performed as the first stage of a fuel fabrication plant. |
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0B003.h |
Systems for the conversion of UF6 to UF4; |
TLB7.1.8 |
Especially designed or prepared systems for the conversion of UF6 to UF4 EXPLANATORY NOTE Conversion of UF6 to UF4 is performed by reduction with hydrogen. |
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0B003.i |
Systems for the conversion of UO2 to UCl4. |
TLB7.1.9 |
Especially designed or prepared systems for the conversion of UO2 to UCl4 EXPLANATORY NOTE Conversion of UO2 to UCl4 can be performed by one of two processes. In the first, UO2 is reacted with carbon tetrachloride (CCl4) at approximately 400 °C. In the second, UO2 is reacted at approximately 700 °C in the presence of carbon black (CAS 1333-86-4), carbon monoxide, and chlorine to yield UCl4. |
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0B004 |
Plant for the production or concentration of heavy water, deuterium and deuterium compounds and specially designed or prepared equipment and components therefor, as follows: |
TLB6 |
Plants for the production or concentration of heavy water, deuterium and deuterium compounds and equipment especially designed or prepared therefor: |
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0B004.a |
Plant for the production of heavy water, deuterium or deuterium compounds, as follows:
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0B004.b |
Equipment and components, as follows: |
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TLB6.1 |
Water — Hydrogen Sulphide Exchange Towers Exchange towers with diameters of 1,5 m or greater and capable of operating at pressures greater than or equal to 2 MPa (300 psi), especially designed or prepared for heavy water production utilizing the water-hydrogen sulphide exchange process. |
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TLB6.2 |
Blowers and Compressors Single stage, low head (i.e., 0,2 MPa or 30 psi) centrifugal blowers or compressors for hydrogen-sulphide gas circulation (i.e., gas containing more than 70 % H2S) especially designed or prepared for heavy water production utilizing the water-hydrogen sulphide exchange process. These blowers or compressors have a throughput capacity greater than or equal to 56 m3/second (120 000 SCFM) while operating at pressures greater than or equal to 1,8 MPa (260 psi) suction and have seals designed for wet H2S service. |
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TLB6.3 |
Ammonia-Hydrogen Exchange Towers Ammonia-hydrogen exchange towers greater than or equal to 35 m (114,3 ft) in height with diameters of 1,5 m (4,9 ft) to 2,5 m (8,2 ft) capable of operating at pressures greater than 15 MPa (2 225 psi) especially designed or prepared for heavy water production utilizing the ammonia-hydrogen exchange process. These towers also have at least one flanged, axial opening of the same diameter as the cylindrical part through which the tower internals can be inserted or withdrawn. |
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TLB6.4 |
Tower Internals and Stage Pumps Tower internals and stage pumps especially designed or prepared for towers for heavy water production utilizing the ammonia-hydrogen exchange process. Tower internals include especially designed stage contactors which promote intimate gas/liquid contact. Stage pumps include especially designed submersible pumps for circulation of liquid ammonia within a contacting stage internal to the stage towers. |
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TLB6.5 |
Ammonia Crackers Ammonia crackers with operating pressures greater than or equal to 3 MPa (450 psi) especially designed or prepared for heavy water production utilizing the ammoniahydrogen exchange process. |
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TLB6.6 |
Infrared Absorption Analyzers Infrared absorption analyzers capable of “on-line” hydrogen/deuterium ratio analysis where deuterium concentrations are equal to or greater than 90 %. |
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|
TLB6.7 |
Catalytic Burners Catalytic burners for the conversion of enriched deuterium gas into heavy water especially designed or prepared for heavy water production utilizing the ammoniahydrogen exchange process. |
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|
TLB6.8 |
Complete heavy water upgrade systems or columns therefor Complete heavy water upgrade systems, or columns therefor, especially designed or prepared for the upgrade of heavy water to reactor-grade deuterium concentration. EXPLANATORY NOTE These systems, which usually employ water distillation to separate heavy water from light water, are especially designed or prepared to produce reactor-grade heavy water (i.e., typically 99,75 % deuterium oxide) from heavy water feedstock of lesser concentration. |
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TLB6.9 |
Ammonia synthesis converters or synthesis units Ammonia synthesis converters or synthesis units especially designed or prepared for heavy water production utilizing the ammonia-hydrogen exchange process. EXPLANATORY NOTE These converters or units take synthesis gas (nitrogen and hydrogen) from an ammonia/hydrogen high-pressure exchange column (or columns), and the synthesized ammonia is returned to the exchange column (or columns). |
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0B005 |
Plant specially designed for the fabrication of “nuclear reactor” fuel elements and specially designed or prepared equipment therefor. Technical Note: Specially designed or prepared equipment for the fabrication of “nuclear reactor” fuel elements includes equipment which:
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Plants for the fabrication of nuclear reactor fuel elements, and equipment especially designed or prepared therefor INTRODUCTORY NOTE Nuclear fuel elements are manufactured from one or more of the source or special fissionable materials mentioned in MATERIAL AND EQUIPMENT of this annex. For oxide fuels, the most common type of fuel, equipment for pressing pellets, sintering, grinding and grading will be present. Mixed oxide fuels are handled in glove boxes (or equivalent containment) until they are sealed in the cladding. In all cases, the fuel is hermetically sealed inside a suitable cladding which is designed to be the primary envelope encasing the fuel so as to provide suitable performance and safety during reactor operation. Also, in all cases, precise control of processes, procedures and equipment to extremely high standards is necessary in order to ensure predictable and safe fuel performance. EXPLANATORY NOTE Items of equipment that are considered to fall within the meaning of the phrase “and equipment especially designed or prepared” for the fabrication of fuel elements include equipment which: (a) normally comes in direct contact with, or directly processes, or controls, the production flow of nuclear material; (b) seals the nuclear material within the cladding; (c) checks the integrity of the cladding or the seal; (d) checks the finish treatment of the sealed fuel; or (e) is used for assembling reactor fuel elements. Such equipment or systems of equipment may include, for example: 1) fully automatic pellet inspection stations especially designed or prepared for checking final dimensions and surface defects of the fuel pellets; 2) automatic welding machines especially designed or prepared for welding end caps onto the fuel pins (or rods); 3) automatic test and inspection stations especially designed or prepared for checking the integrity of completed fuel pins (or rods); 4) systems especially designed or prepared to manufacture nuclear fuel cladding. Item 3 typically includes equipment for: a) x-ray examination of pin (or rod) end cap welds, b) helium leak detection from pressurized pins (or rods), and c) gamma-ray scanning of the pins (or rods) to check for correct loading of the fuel pellets inside. |
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0B006 |
Plant for the reprocessing of irradiated “nuclear reactor” fuel elements, and specially designed or prepared equipment and components therefor.
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TLB3 |
Plants for the reprocessing of irradiated fuel elements, and equipment especially designed or prepared therefor INTRODUCTORY NOTE Reprocessing irradiated nuclear fuel separates plutonium and uranium from intensely radioactive fission products and other transuranic elements. Different technical processes can accomplish this separation. However, over the years Purex has become the most commonly used and accepted process. Purex involves the dissolution of irradiated nuclear fuel in nitric acid, followed by separation of the uranium, plutonium, and fission products by solvent extraction using a mixture of tributyl phosphate in an organic diluent. Purex facilities have process functions similar to each other, including: irradiated fuel element chopping, fuel dissolution, solvent extraction, and process liquor storage. There may also be equipment for thermal denitration of uranium nitrate, conversion of plutonium nitrate to oxide or metal, and treatment of fission product waste liquor to a form suitable for long term storage or disposal. However, the specific type and configuration of the equipment performing these functions may differ between Purex facilities for several reasons, including the type and quantity of irradiated nuclear fuel to be reprocessed and the intended disposition of the recovered materials, and the safety and maintenance philosophy incorporated into the design of the facility. A “plant for the reprocessing of irradiated fuel elements”, includes the equipment and components which normally come in direct contact with and directly control the irradiated fuel and the major nuclear material and fission product processing streams. These processes, including the complete systems for plutonium conversion and plutonium metal production, may be identified by the measures taken to avoid criticality (e.g. by geometry), radiation exposure (e.g. by shielding), and toxicity hazards (e.g. by containment). |
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TLB3.1 |
Irradiated fuel element chopping machines Remotely operated equipment especially designed or prepared for use in a reprocessing plant as identified above and intended to cut, chop or shear irradiated nuclear fuel assemblies, bundles or rods. EXPLANATORY NOTE This equipment breaches the cladding of the fuel to expose the irradiated nuclear material to dissolution. Especially designed metal cutting shears are the most commonly employed, although advanced equipment, such as lasers, may be used. |
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TLB3.2 |
Dissolvers Critically safe tanks (e.g. small diameter, annular or slab tanks) especially designed or prepared for use in a reprocessing plant as identified above, intended for dissolution of irradiated nuclear fuel and which are capable of withstanding hot, highly corrosive liquid, and which can be remotely loaded and maintained. EXPLANATORY NOTE Dissolvers normally receive the chopped-up spent fuel. In these critically safe vessels, the irradiated nuclear material is dissolved in nitric acid and the remaining hulls removed from the process stream. |
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TLB3.3 |
Solvent extractors and solvent extraction equipment Especially designed or prepared solvent extractors such as packed or pulse columns, mixer settlers or centrifugal contactors for use in a plant for the reprocessing of irradiated fuel. Solvent extractors must be resistant to the corrosive effect of nitric acid. Solvent extractors are normally fabricated to extremely high standards (including special welding and inspection and quality assurance and quality control techniques) out of low carbon stainless steels, titanium, zirconium, or other high quality materials. EXPLANATORY NOTE Solvent extractors both receive the solution of irradiated fuel from the dissolvers and the organic solution which separates the uranium, plutonium, and fission products. Solvent extraction equipment is normally designed to meet strict operating parameters, such as long operating lifetimes with no maintenance requirements or adaptability to easy replacement, simplicity of operation and control, and flexibility for variations in process conditions. |
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TLB3.4 |
Chemical holding or storage vessels Especially designed or prepared holding or storage vessels for use in a plant for the reprocessing of irradiated fuel. The holding or storage vessels must be resistant to the corrosive effect of nitric acid. The holding or storage vessels are normally fabricated of materials such as low carbon stainless steels, titanium or zirconium, or other high quality materials. Holding or storage vessels may be designed for remote operation and maintenance and may have the following features for control of nuclear criticality:
EXPLANATORY NOTE Three main process liquor streams result from the solvent extraction step. Holding or storage vessels are used in the further processing of all three streams, as follows:
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TLB3.5 |
Neutron measurement systems for process control Neutron measurement systems especially designed or prepared for integration and use with automated process control systems in a plant for the reprocessing of irradiated fuel elements. EXPLANATORY NOTE These systems involve the capability of active and passive neutron measurement and discrimination in order to determine the fissile material quantity and composition. The complete system is composed of a neutron generator, a neutron detector, amplifiers, and signal processing electronics. The scope of this entry does not include neutron detection and measurement instruments that are designed for nuclear material accountancy and safeguarding or any other application not related to integration and use with automated process control systems in a plant for the reprocessing of irradiated fuel elements. |
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0B007 |
Plant for the conversion of plutonium and equipment specially designed or prepared therefor, as follows: |
TLB7.2.1 |
Especially designed or prepared systems for the conversion of plutonium nitrate to oxide |
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0B007.a |
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EXPLANATORY NOTE The main functions involved in this process are: process feed storage and adjustment, precipitation and solid/liquor separation, calcination, product handling, ventilation, waste management, and process control. The process systems are particularly adapted so as to avoid criticality and radiation effects and to minimize toxicity hazards. In most reprocessing facilities, this process involves the conversion of plutonium nitrate to plutonium dioxide. Other processes can involve the precipitation of plutonium oxalate or plutonium peroxide. |
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0B007.b |
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TLB7.2.2 |
Especially designed or prepared systems for plutonium metal production EXPLANATORY NOTE This process usually involves the fluorination of plutonium dioxide, normally with highly corrosive hydrogen fluoride, to produce plutonium fluoride which is subsequently reduced using high purity calcium metal to produce metallic plutonium and a calcium fluoride slag. The main functions involved in this process are fluorination (e.g. involving equipment fabricated or lined with a precious metal), metal reduction (e.g. employing ceramic crucibles), slag recovery, product handling, ventilation, waste management and process control. The process systems are particularly adapted so as to avoid criticality and radiation effects and to minimize toxicity hazards. Other processes include the fluorination of plutonium oxalate or plutonium peroxide followed by a reduction to metal. |
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0C001 |
“Natural uranium” or “depleted uranium” or thorium in the form of metal, alloy, chemical compound or concentrate and any other material containing one or more of the foregoing;
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TLA.1.1 |
1.1. “Source material” The term “source material” means uranium containing the mixture of isotopes occurring in nature; uranium depleted in the isotope 235; thorium; any of the foregoing in the form of metal, alloy, chemical compound, or concentrate; any other material containing one or more of the foregoing in such concentration as the Board of Governors shall from time to time determine; and such other material as the Board of Governors shall from time to time determine. |
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0C002 |
“Special fissile materials”
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TLA.1.2 |
1.2. “Special fissionable material”
However, for the purposes of the Guidelines, items specified in subparagraph (a) below, and exports of source or special fissionable material to a given recipient country, within a period of 12 months, below the limits specified in subparagraph (b) below, shall not be included:
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0C003 |
Deuterium, heavy water (deuterium oxide) and other compounds of deuterium, and mixtures and solutions containing deuterium, in which the isotopic ratio of deuterium to hydrogen exceeds 1:5 000 . |
TLB2.1 |
2.1. Deuterium and heavy water Deuterium, heavy water (deuterium oxide) and any other deuterium compound in which the ratio of deuterium to hydrogen atoms exceeds 1:5 000 for use in a nuclear reactor as defined in paragraph 1.1. above in quantities exceeding 200 kg of deuterium atoms for any one recipient country in any period of 12 months. |
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0C004 |
Graphite having a purity level better than 5 parts per million ‘boron equivalent’ and with a density greater than 1,50 g/cm3 for use in a “nuclear reactor”, in quantities exceeding 1 kg.
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TLB2.2 |
2.2. Nuclear grade graphite Graphite having a purity level better than 5 parts per million boron equivalent and with a density greater than 1,50 g/cm3 for use in a nuclear reactor as defined in paragraph 1.1 above, in quantities exceeding 1 kilogram. EXPLANATORY NOTE For the purpose of export control, the Government will determine whether or not the exports of graphite meeting the above specifications are for nuclear reactor use. Boron equivalent (BE) may be determined xperimentally or is calculated as the sum of BEz for impurities (excluding BEcarbon since carbon is not considered an impurity) including boron, where:
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0C005 |
Specially prepared compounds or powders for the manufacture of gaseous diffusion barriers, resistant to corrosion by UF6 (e.g. nickel or alloy containing 60 weight per cent or more nickel, aluminium oxide and fully fluorinated hydrocarbon polymers), having a purity of 99,9 % by weight or more and a particle size less than 10 μm measured by American Society for Testing and Materials (ASTM) B330 standard and a high degree of particle size uniformity. |
TLB5.3.1b |
Gaseous diffusion barriers and barrier materials
Such compounds and powders include nickel or alloys containing 60 % or more nickel, aluminium oxide, or UF6-resistant fully fluorinated hydrocarbon polymers having a purity of 99,9 % by weight or more, a particle size less than 10 μm, and a high degree of particle size uniformity, which are especially prepared for the manufacture of gaseous diffusion barriers. |
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OD001 |
T*“Software” specially designed or modified for the “development”, “production” or “use” of goods specified in this Category. II* IV* |
TLB* |
“software” means a collection of one or more “programs” or “microprograms” fixed in any tangible medium of expression. “technical assistance” may take forms such as: instruction, skills, training, working knowledge, consulting services. |
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0E001 |
T* “Technology” according to the Nuclear Technology Note for the “development”, “production” or “use” of goods specified in this Category. II* IV |
TLB* |
“technology” means specific information required for the “development”, “production”, or “use” of any item contained in the List. This information may take the form of “technical data”, or “technical assistance”. |
CATEGORY 1 — SPECIAL MATERIALS AND RELATED EQUIPMENT
1A Systems, Equipment and Components
The corresponding systems, equipment and components as identified in Council Regulation (EC) No 428/2009 of 5 May 2009 setting up a Community regime for the control of exports, transfer, brokering and transit of dual-use items |
Nuclear Suppliers Group's control list as in INFCIRC/254/Rev.9/Part 2 |
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1A007 |
Technical Notes:
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6.A.1. |
Detonators and multipoint initiation systems, as follows:
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1A007 |
Equipment and devices, specially designed to initiate charges and devices containing “energetic materials”, by electrical means, as follows:
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6.A.2. |
Firing sets and equivalent high-current pulse generators, as follows:
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1A202 |
Composite structures, other than those specified in 1A002, in the form of tubes and having both of the following characteristics:
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2.A.3. |
Composite structures in the form of tubes having both of the following characteristics:
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1A225 |
Platinized catalysts specially designed or prepared for promoting the hydrogen isotope exchange reaction between hydrogen and water for the recovery of tritium from heavy water or for the production of heavy water. |
2.A.2. |
Platinized catalysts specially designed or prepared for promoting the hydrogen isotope exchange reaction between hydrogen and water for the recovery of tritium from heavy water or for the production of heavy water. |
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1A226 |
Specialized packings which may be used in separating heavy water from ordinary water, having both of the following characteristics:
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4.A.1. |
Specialized packings which may be used in separating heavy water from ordinary water, having both of the following characteristics:
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1A227 |
High-density (lead glass or other) radiation shielding windows, having all of the following characteristics, and specially designed frames therefor:
Technical Note: In 1A227 the term ‘cold area’ means the viewing area of the window exposed to the lowest level of radiation in the design application. |
1.A.1. |
High-density (lead glass or other) radiation shielding windows, having all of the following characteristics, and specially designed frames therefor:
Technical Note: In Item 1.A.1.a. the term ‘cold area’ means the viewing area of the window exposed to the lowest level of radiation in the design application. |
1B Test, Inspection and Production Equipment
The corresponding systems, equipment and components as identified in Council Regulation (EC) No 428/2009 of 5 May 2009 setting up a Community regime for the control of exports, transfer, brokering and transit of dual-use items |
Nuclear Suppliers Group's control list as in INFCIRC/254/Rev.9/Part 2 |
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1B201 |
Filament winding machines, other than those specified in 1B001 or 1B101, and related equipment, as follows:
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3.B.4. |
Filament winding machines and related equipment, as follows:
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1B225 |
Electrolytic cells for fluorine production with an output capacity greater than 250 g of fluorine per hour. |
3.B.1. |
Electrolytic cells for fluorine production with an output capacity greater than 250 g of fluorine per hour. |
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1B226 |
Electromagnetic isotope separators designed for, or equipped with, single or multiple ion sources capable of providing a total ion beam current of 50 mA or greater.
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3.B.5. |
Electromagnetic isotope separators designed for, or equipped with, single or multiple ion sources capable of providing a total ion beam current of 50 mA or greater. Notes:
Technical Note: A single 50 mA ion source cannot produce more than 3 g of separated highly enriched uranium (HEU) per year from natural abundance feed. |
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1B228 |
Hydrogen-cryogenic distillation columns having all of the following characteristics:
Technical Note: In 1B228 ‘effective length’ means the active height of packing material in a packed-type column, or the active height of internal contactor plates in a plate-type column. |
4.B.2. |
Hydrogen-cryogenic distillation columns having all of the following characteristics:
Technical Note: The term ‘effective length’ means the active height of packing material in a packed-type column, or the active height of internal contactor plates in a plate-type column. |
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1B229 |
Water-hydrogen sulphide exchange tray columns and ‘internal contactors’, as follows:
Technical Note: ‘Internal contactors’ of the columns are segmented trays which have an effective assembled diameter of 1,8 m or greater, are designed to facilitate countercurrent contacting and are constructed of stainless steels with a carbon content of 0,03 % or less. These may be sieve trays, valve trays, bubble cap trays, or turbogrid trays. |
4.B.1. |
Water-hydrogen sulfide exchange tray columns and internal contactors, as follows:
Technical Note: Internal contactors of the columns are segmented trays which have an effective assembled diameter of 1,8 m or greater; are designed to facilitate countercurrent contacting and are constructed of stainless steels with a carbon content of 0,03 % or less. These may be sieve trays, valve trays, bubble cap trays or turbogrid trays. |
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1B230 |
Pumps capable of circulating solutions of concentrated or dilute potassium amide catalyst in liquid ammonia (KNH2/NH3), having all of the following characteristics:
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4.A.2. |
Pumps capable of circulating solutions of concentrated or dilute potassium amide catalyst in liquid ammonia (KNH2/NH3), having all of the following characteristics:
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1B231 |
Tritium facilities or plants, and equipment therefor, as follows:
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2.B.1. |
Tritium facilities or plants, and equipment therefor, as follows:
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1B232 |
Turboexpanders or turboexpander-compressor sets having both of the following characteristics:
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4.A.3. |
Turboexpanders or turboexpander-compressor sets having both of the following characteristics:
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1B233 |
Lithium isotope separation facilities or plants, and systems and equipment therefor, as follows:
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2.B.2. |
Lithium isotope separation facilities or plants, and systems and equipment therefor, as follows:
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1B234 |
High explosive containment vessels, chambers, containers and other similar containment devices designed for the testing of high explosives or explosive devices and having both of the following characteristics:
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5.B.7. |
High explosive containment vessels, chambers, containers and other similar containment devices designed for the testing of high explosives or explosive devices and having both of the following characteristics:
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1C Materials
The corresponding systems, equipment and components as identified in Council Regulation (EC) No 428/2009 of 5 May 2009 setting up a Community regime for the control of exports, transfer, brokering and transit of dual-use items |
Nuclear Suppliers Group's control list as in INFCIRC/254/Rev.9/Part 2 |
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1C202 |
Alloys, other than those specified in 1C002.b.3. or .b.4., as follows:
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2.C.1. |
Aluminium alloys having both of the following characteristics:
Technical Note: In Item 2.C.1. the phrase ‘capable of’ encompasses aluminium alloys before or after heat treatment. |
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1C202 |
Technical Note: The phrase alloys ‘capable of’ encompasses alloys before or after heat treatment. |
2.C.13. |
Titanium alloys having both of the following characteristics:
In the form of tubes or cylindrical solid forms (including forgings) with an outside diameter of more than 75 mm. Technical Note: In Item 2.C.13. the phrase ‘capable of’ encompasses titanium alloys before or after heat treatment |
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1C210 |
‘Fibrous or filamentary materials’ or prepregs, other than those specified in 1C010.a., b. or e., as follows:
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2.C.7.a |
“Fibrous or filamentary materials”, and prepregs, as follows:
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2.C.7.b |
Glass “fibrous or filamentary materials” having both of the following characteristics:
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Technical Note: The resin forms the matrix of the composite.
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2.C.7.c |
Technical Note: The resin forms the matrix of the composite. Technical Notes:
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1C216 |
Maraging steel, other than that specified in 1C116, ‘capable of’ an ultimate tensile strength of 1 950 MPa or more, at 293 K (20 °C).
Technical Note: The phrase maraging steel ‘capable of’ encompasses maraging steel before or after heat treatment. |
2.C.11. |
Maraging steel ‘capable of’ an ultimate tensile strength of 1 950 MPa or more at 293 K (20 °C).
Technical Note: In Item 2.C.11. the phrase ‘capable of’ encompasses maraging steel before or after heat treatment. |
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1C225 |
Boron enriched in the boron-10 (10B) isotope to greater than its natural isotopic abundance, as follows: elemental boron, compounds, mixtures containing boron, manufactures thereof, waste or scrap of any of the foregoing.
Technical Note: The natural isotopic abundance of boron-10 is approximately 18,5 weight per cent (20 atom per cent). |
2.C.4. |
Boron enriched in the boron-10 (10B) isotope to greater than its natural isotopic abundance, as follows: elemental boron, compounds, mixtures containing boron, manufactures thereof, waste or scrap of any of the foregoing.
Technical Note: The natural isotopic abundance of boron-10 is approximately 18,5 weight percent (20 atom percent). |
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1C226 |
Tungsten, tungsten carbide, and alloys containing more than 90 % tungsten by weight, other than that specified by 1C117, having both of the following characteristics:
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2.C.14. |
Tungsten, tungsten carbide, and alloys containing more than 90 % tungsten by weight, having both of the following characteristics:
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1C227 |
Calcium having both of the following characteristics:
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2.C.5. |
Calcium having both of the following characteristics:
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1C228 |
Magnesium having both of the following characteristics:
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2.C.10. |
Magnesium having both of the following characteristics:
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1C229 |
Bismuth having both of the following characteristics:
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2.C.3. |
Bismuth having both of the following characteristics:
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1C230 |
Beryllium metal, alloys containing more than 50 % beryllium by weight, beryllium compounds, manufactures thereof, and waste or scrap of any of the foregoing, other than that specified in the Military Goods Controls.
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2.C.2. |
Beryllium metal, alloys containing more than 50 % beryllium by weight, beryllium compounds, manufactures thereof, and waste or scrap of any of the foregoing.
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1C231 |
Hafnium metal, alloys containing more than 60 % hafnium by weight, hafnium compounds containing more than 60 % hafnium by weight, manufactures thereof, and waste or scrap of any of the foregoing. |
2.C.8. |
Hafnium metal, alloys containing more than 60 % hafnium by weight, hafnium compounds containing more than 60 % hafnium by weight, manufactures thereof, and waste or scrap of any of the foregoing. |
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1C232 |
Helium-3 (3He), mixtures containing helium-3, and products or devices containing any of the foregoing.
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2.C.18. |
Helium-3 (3He), mixtures containing helium-3, and products or devices containing any of the foregoing.
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1C233 |
Lithium enriched in the lithium-6 (6Li) isotope to greater than its natural isotopic abundance, and products or devices containing enriched lithium, as follows: elemental lithium, alloys, compounds, mixtures containing lithium, manufactures thereof, waste or scrap of any of the foregoing.
Technical Note: The natural isotopic abundance of lithium-6 is approximately 6,5 weight per cent (7,5 atom per cent). |
2.C.9. |
Lithium enriched in the lithium-6 (6Li) isotope to greater than its natural isotopic abundance and products or devices containing enriched lithium, as follows: elemental lithium, alloys, compounds, mixtures containing lithium, manufactures thereof, waste or scrap of any of the foregoing.
Technical Note: The natural isotopic abundance of lithium-6 is approximately 6,5 weight percent (7,5 atom percent). |
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1C234 |
Zirconium with a hafnium content of less than 1 part hafnium to 500 parts zirconium by weight, as follows: metal, alloys containing more than 50 % zirconium by weight, compounds, manufactures thereof, waste or scrap of any of the foregoing, other than those specified in 0A001.f.
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2.C.15. |
Zirconium with a hafnium content of less than 1 part hafnium to 500 parts zirconium by weight, as follows: metal, alloys containing more than 50 % zirconium by weight, compounds, manufactures thereof, waste or scrap of any of the foregoing.
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1C235 |
Tritium, tritium compounds, mixtures containing tritium in which the ratio of tritium to hydrogen atoms exceeds 1 part in 1 000 , and products or devices containing any of the foregoing.
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2.C.17. |
Tritium, tritium compounds, mixtures containing tritium in which the ratio of tritium to hydrogen atoms exceeds 1 part in 1 000 , and products or devices containing any of the foregoing.
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1C236 |
‘Radionuclides’ appropriate for making neutron sources based on alpha-n reaction, other than those specified in 0C001 and 1C012.a., in the following forms:
Technical Note: In 1C236 ‘radionuclides’ are any of the following:
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2.C.19. |
Radionuclides appropriate for making neutron sources based on alpha-n reaction:
In the following forms:
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1C237 |
Radium 226 (226Ra), radium-226 alloys, radium-226 compounds, mixtures containing radium 226, manufactures thereof, and products or devices containing any of the foregoing.
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2.C.12. |
Radium-226 (226Ra), radium-226 alloys, radium-226 compounds, mixtures containing radium-226, manufactures thereof, and products or devices containing any of the foregoing.
|
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1C238 |
Chlorine trifluoride (ClF3). |
2.C.6. |
Chlorine trifluoride (ClF3). |
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1C239 |
High explosives, other than those specified in the Military Goods Controls, or substances or mixtures containing more than 2 % by weight thereof, with a crystal density greater than 1,8 g/cm3 and having a detonation velocity greater than 8 000 m/s. |
6.C.1.o |
Any explosive with a crystal density greater than 1,8 g/cm3 and having a detonation velocity greater than 8 000 m/s. |
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1C240 |
Nickel powder and porous nickel metal, other than those specified in 0C005, as follows:
Technical Note: 1C240.b. refers to porous metal formed by compacting and sintering the materials in 1C240.a. to form a metal material with fine pores interconnected throughout the structure. |
2.C.16. |
Nickel powder and porous nickel metal, as follows:
Technical Note: Item 2.C.16.b. refers to porous metal formed by compacting and sintering the material in Item 2.C.16.a. to form a metal material with fine pores interconnected throughout the structure. |
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1C241 |
Rhenium, and alloys containing 90 % by weight or more rhenium; and alloys of rhenium and tungsten containing 90 % by weight or more of any combination of rhenium and tungsten, other than those specified in 1C226, having both of the following characteristics:
|
2.C.20. |
Rhenium, and alloys containing 90 % by weight or more rhenium; and alloys of rhenium and tungsten containing 90 % by weight or more of any combination of rhenium and tungsten, having both of the following characteristics:
|
1D Software
The corresponding systems, equipment and components as identified in Council Regulation (EC) No 428/2009 of 5 May 2009 setting up a Community regime for the control of exports, transfer, brokering and transit of dual-use items |
Nuclear Suppliers Group's control list as in INFCIRC/254/Rev.9/Part 2 |
||
1D001 |
“Software” specially designed or modified for the “development”, “production” or “use” of equipment specified in 1B001 to 1B003. |
1.D.2. |
“software” means a collection of one or more “programs” or “microprograms” fixed in any tangible medium of expression |
1D201 |
“Software” specially designed for the “use” of goods specified in 1B201. |
1.D.3. |
“software” means a collection of one or more “programs” or “microprograms” fixed in any tangible medium of expression |
1E Technology
The corresponding systems, equipment and components as identified in Council Regulation (EC) No 428/2009 of 5 May 2009 setting up a Community regime for the control of exports, transfer, brokering and transit of dual-use items |
Nuclear Suppliers Group's control list as in INFCIRC/254/Rev.9/Part 2 |
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1E201 |
“Technology” according to the General Technology Note for the “use” of goods specified in 1A002, 1A007, 1A202, 1A225 to 1A227, 1B201, 1B225 to 1B234, 1C002.b.3. or .b.4., 1C010.b., 1C202, 1C210, 1C216, 1C225 to 1C241 or 1D201. |
1.E.1. |
“Technology” -- means specific information required for the “development”, “production”, or “use” of any item contained in the List. This information may take the form of “technical data” or “technical assistance”. |
1E202 |
“Technology” according to the General Technology Note for the “development” or “production” of goods specified in 1A007, 1A202 or 1A225 to 1A227. |
1.E.1. |
“Technology” -- means specific information required for the “development”, “production”, or “use” of any item contained in the List. This information may take the form of “technical data” or “technical assistance”. |
1E203 |
“Technology” according to the General Technology Note for the “development” or “production” of goods specified in 1A007, 1A202 or 1A225 to 1A227. |
1.E.1. |
“Technology” -- means specific information required for the “development”, “production”, or “use” of any item contained in the List. This information may take the form of “technical data” or “technical assistance”. |
CATEGORY 2 — MATERIALS PROCESSING
2A Systems, Equipment and Components
The corresponding systems, equipment and components as identified in Council Regulation (EC) No 428/2009 of 5 May 2009 setting up a Community regime for the control of exports, transfer, brokering and transit of dual-use items |
Nuclear Suppliers Group's control list as in INFCIRC/254/Rev.9/Part 2 |
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2A225 |
Crucibles made of materials resistant to liquid actinide metals, as follows:
|
2.A.1 |
Crucibles made of materials resistant to liquid actinide metals, as follows:
|
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2A226 |
Valves having all of the following characteristics:
Technical Note: For valves with different inlet and outlet diameters, the ‘nominal size’ in 2A226 refers to the smallest diameter. |
3.A.3. |
Valves having all of the following characteristics:
Technical Note: For valves with different inlet and outlet diameter, the nominal size parameter in Item 3.A.3.a. refers to the smallest diameter. |
2B Test, Inspection and Production Equipment
The corresponding systems, equipment and components as identified in Council Regulation (EC) No 428/2009 of 5 May 2009 setting up a Community regime for the control of exports, transfer, brokering and transit of dual-use items |
Nuclear Suppliers Group's control list as in INFCIRC/254/Rev.9/Part 2 |
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2B001 |
Machine tools and any combination thereof, for removing (or cutting) metals, ceramics or “composites”, which, according to the manufacturer's technical specification, can be equipped with electronic devices for “numerical control”, as follows:
|
1.B.2. |
Machine tools, as follows, and any combination thereof, for removing or cutting metals, ceramics, or composites, which, according to the manufacturer's technical specifications, can be equipped with electronic devices for simultaneous “contouring control” in two or more axes:
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2B006 |
Dimensional inspection or measuring systems, equipment and “electronic assemblies”, as follows: |
1.B.3. |
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2B006.b. |
Linear and angular displacement measuring instruments, as follows: |
1.B.3. |
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2B006.b. |
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1.B.3.b. |
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2B006.b. |
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1.B.3.c |
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2B116 |
Vibration test systems, equipment and components therefor, as follows:
Technical Note: In 2B116, ‘bare table’ means a flat table, or surface, with no fixture or fittings. |
1.B.6. |
Vibration test systems, equipment, and components as follows:
Technical Note: In Item 1.B.6. “bare table” means a flat table, or surface, with no fixtures or fittings. |
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2B201 |
Machine tools and any combination thereof, other than those specified in 2B001, as follows, for removing or cutting metals, ceramics or “composites”, which, according to the manufacturer's technical specification, can be equipped with electronic devices for simultaneous “contouring control” in two or more axes: Technical Notes: Stated ‘positioning accuracy’ levels derived under the following procedures from measurements made according to ISO 230/2 (1988) (2) or national equivalents may be used for each machine tool model if provided to, and accepted by, national authorities instead of individual machine tests. Stated ‘positioning accuracy’ are to be derived as follows:
|
1.B.2. |
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2B201. |
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1.B.2.b |
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2B201 |
|
1.B.2.c |
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2B204 |
“Isostatic presses”, other than those specified in 2B004 or 2B104, and related equipment, as follows:
Technical Note: In 2B204 the inside chamber dimension is that of the chamber in which both the working temperature and the working pressure are achieved and does not include fixtures. That dimension will be the smaller of either the inside diameter of the pressure chamber or the inside diameter of the insulated furnace chamber, depending on which of the two chambers is located inside the other. |
1.B.5. |
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2B206 |
Dimensional inspection machines, instruments or systems, other than those specified in 2B006, as follows: |
1.B.3. |
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2B206. |
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1.B.3.a |
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2B206. |
Technical Notes: All parameters of measurement values in 2B206 represent plus/minus i.e., not total band. |
1.B.3.d |
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2B207 |
“Robots”, “end-effectors” and control units, other than those specified in 2B007, as follows:
|
1.A.3.a1 |
‘Robots’, ‘end-effectors’ and control units as follows: a. ‘Robots’ or ‘end-effectors’ having either of the following characteristics: 1. Specially designed to comply with national safety standards applicable to handling high explosives (for example, meeting electrical code ratings for high explosives); |
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1.A.3.b |
Control units specially designed for any of the ‘robots’ or ‘end-effectors’ specified in Item 1.A.3.a.
Technical Notes:
|
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2B209 |
Flow forming machines, spin forming machines capable of flow forming functions, other than those specified in 2B009 or 2B109, and mandrels, as follows:
|
1.B.1. |
Flow-forming machines, spin-forming machines capable of flow-forming functions, and mandrels, as follows:
|
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2B219 |
Centrifugal multiplane balancing machines, fixed or portable, horizontal or vertical, as follows:
|
3.B.3. |
Centrifugal multiplane balancing machines, fixed or portable, horizontal or vertical, as follows:
|
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2B225 |
Remote manipulators that can be used to provide remote actions in radiochemical separation operations or hot cells, having either of the following characteristics:
Technical Note: Remote manipulators provide translation of human operator actions to a remote operating arm and terminal fixture. They may be of ‘master/slave’ type or operated by joystick or keypad. |
1.A.4. |
Remote manipulators that can be used to provide remote actions in radiochemical separation operations or hot cells, having either of the following characteristics:
Technical Note: Remote manipulators provide translation of human operator actions to a remote operating arm and terminal fixture. They may be of a master/slave type or operated by joystick or keypad. |
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2B226 |
Controlled atmosphere (vacuum or inert gas) induction furnaces, and power supplies therefor, as follows:
|
1.B.4. |
Controlled atmosphere (vacuum or inert gas) induction furnaces, and power supplies therefor, as follows:
|
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2B227 |
Vacuum or other controlled atmosphere metallurgical melting and casting furnaces and related equipment as follows:
|
1.B.7. |
Vacuum or other controlled atmosphere metallurgical melting and casting furnaces and related equipment, as follows:
|
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2B228 |
Rotor fabrication or assembly equipment, rotor straightening equipment, bellows-forming mandrels and dies, as follows:
|
3.B.2. |
Rotor fabrication or assembly equipment, rotor straightening equipment, bellows-forming mandrels and dies, as follows:
|
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2B230 |
All types of ‘pressure transducers’ capable of measuring absolute pressures and having all of the following:
Technical Notes:
|
3.A.7. |
All types of pressure transducers capable of measuring absolute pressures and having all of the following characteristics:
Notes:
|
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2B231 |
Vacuum pumps having all of the following characteristics:
Technical Notes:
|
3.A.8. |
Vacuum pumps having all of the following characteristics:
Technical Notes:
|
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2B232 |
High-velocity gun systems (propellant, gas, coil, electromagnetic, and electrothermal types, and other advanced systems) capable of accelerating projectiles to 1,5 km/s or greater.
|
5.B.2. |
High-velocity gun systems (propellant, gas, coil, electromagnetic, and electrothermal types, and other advanced systems) capable of accelerating projectiles to 1,5 km/s or greater.
|
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2B233 |
Bellows-sealed scroll-type compressors and bellows-sealed scroll-type vacuum pumps having all of the following:
|
3.A.9. |
Bellows-sealed scroll-type compressors and bellows-sealed scroll-type vacuum pumps having all of the following characteristics:
Technical Notes:
|
2D Software
The corresponding systems, equipment and components as identified in Council Regulation (EC) No 428/2009 of 5 May 2009 setting up a Community regime for the control of exports, transfer, brokering and transit of dual-use items |
Nuclear Suppliers Group's control list as in INFCIRC/254/Rev.9/Part 2 |
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2D001 |
“Software”, other than that specified in 2D002, as follows:
|
1.D.2. |
“Software” specially designed or modified for the “use” of equipment specified in Item 1.A.3., 1.B.1., 1.B.3., 1.B.5., 1.B.6.a., 1.B.6.b., 1.B.6.d. or 1.B.7.
|
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2D002 |
“Software” for electronic devices, even when residing in an electronic device or system, enabling such devices or systems to function as a “numerical control” unit, capable of co-ordinating simultaneously more than four axes for “contouring control”.
|
1.D.3. |
“Software” for any combination of electronic devices or system enabling such device(s) to function as a “numerical control” unit for machine tools, that is capable of controlling five or more interpolating axes that can be coordinated simultaneously for “contouring control”. Notes:
|
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2D101 |
“Software” specially designed or modified for the “use” of equipment specified in 2B104, 2B105, 2B109, 2B116, 2B117 or 2B119 to 2B122.
|
1.D.1. |
“Software” specially designed or modified for the “use” of equipment specified in Item 1.A.3., 1.B.1., 1.B.3., 1.B.5., 1.B.6.a., 1.B.6.b., 1.B.6.d. or 1.B.7.
|
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2D201 |
“Software” specially designed for the “use” of equipment specified in 2B204, 2B206, 2B207, 2B209, 2B219 or 2B227. |
1.D.1. |
“Software” specially designed or modified for the “use” of equipment specified in Item 1.A.3., 1.B.1., 1.B.3., 1.B.5., 1.B.6.a., 1.B.6.b., 1.B.6.d. or 1.B.7.
|
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2D202 |
“Software” specially designed or modified for the “development”, “production” or “use” of equipment specified in 2B201.
|
1.D.2. |
“Software” specially designed or modified for the “development”, “production”, or “use” of equipment specified in Item 1.B.2.
|
2E Technology
The corresponding systems, equipment and components as identified in Council Regulation (EC) No 428/2009 of 5 May 2009 setting up a Community regime for the control of exports, transfer, brokering and transit of dual-use items |
Nuclear Suppliers Group's control list as in INFCIRC/254/Rev.9/Part 2 |
||||
2E001 |
“Technology” according to the General Technology Note for the “development” of equipment or “software” specified in 2A, 2B or 2D.
|
1.E.1 |
“Technology” according to the Technology Controls for the “development”, “production” or “use” of equipment, material or “software” specified in 1.A. through 1.D. |
||
2E002 |
“Technology” according to the General Technology Note for the “production” of equipment specified in 2A or 2B |
1.E.1 |
“Technology” according to the Technology Controls for the “development”, “production” or “use” of equipment, material or “software” specified in 1.A. through 1.D. |
||
2E101 |
“Technology” according to the General Technology Note for the “use” of equipment or “software” specified in 2B004, 2B009, 2B104, 2B109, 2B116, 2B119 to 2B122 or 2D101. |
1.E.1 |
“Technology” according to the Technology Controls for the “development”, “production” or “use” of equipment, material or “software” specified in 1.A. through 1.D. |
||
2E201 |
“Technology” according to the General Technology Note for the “use” of equipment or “software” specified in 2A225, 2A226, 2B001, 2B006, 2B007.b., 2B007.c., 2B008, 2B009, 2B201, 2B204, 2B206, 2B207, 2B209, 2B225 to 2B233, 2D201 or 2D202. |
1.E.1 |
“Technology” according to the Technology Controls for the “development”, “production” or “use” of equipment, material or “software” specified in 1.A. through 1.D. |
CATEGORY 3 — ELECTRONICS
3A Systems, Equipment and Components
The corresponding systems, equipment and components as identified in Council Regulation (EC) No 428/2009 of 5 May 2009 setting up a Community regime for the control of exports, transfer, brokering and transit of dual-use items |
Nuclear Suppliers Group's control list as in INFCIRC/254/Rev.9/Part 2 |
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3A201 |
Electronic components, other than those specified in 3A001, as follows;
|
6.A.4. |
Pulse discharge capacitors having either of the following sets of characteristics:
|
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3A201 |
|
3.A.4. |
Superconducting solenoidal electromagnets having all of the following characteristics:
|
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3A201 |
|
5.B.1. |
Flash X-ray generators or pulsed electron accelerators having either of the following sets of characteristics:
Technical Notes:
|
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3A225 |
Frequency changers or generators, other than those specified in 0B001.b.13., usable as a variable or fixed frequency motor drive, having all of the following characteristics:
Technical Notes:
|
3.A.1. |
Frequency changers or generators, usable as a variable frequency or fixed frequency motor drive, having all of the following characteristics:
Notes:
Technical Notes:
|
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3A226 |
High-power direct current power supplies, other than those specified in 0B001.j.6., having both of the following characteristics:
|
3.A.5. |
High-power direct current power supplies having both of the following characteristics:
|
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3A227 |
High-voltage direct current power supplies, other than those specified in 0B001.j.5., having both of the following characteristics:
|
3.A.6. |
High-voltage direct current power supplies having both of the following characteristics:
|
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3A228 |
Switching devices, as follows:
|
6.A.3. |
Switching devices as follows:
|
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3A229 |
High-current pulse generators as follows:
|
6.A.2. |
Firing sets and equivalent high-current pulse generators, as follows:
|
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3A230 |
High-speed pulse generators, and ‘pulse heads’ therefor, having both of the following characteristics:
Technical Notes:
|
5.B.6. |
High-speed pulse generators, and pulse heads therefor, having both of the following characteristics:
Technical Notes:
|
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3A231 |
Neutron generator systems, including tubes, having both of the following characteristics:
|
6.A.5. |
Neutron generator systems, including tubes, having both of the following characteristics:
|
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3A232 |
Multipoint initiation systems, other than those specified in 1A007, as follows:
|
6.A.1. |
Detonators and multipoint initiation systems, as follows:
Technical Note: In Item 6.A.1. the detonators of concern all utilize a small electrical conductor (bridge, bridge wire, or foil) that explosively vaporizes when a fast, high-current electrical pulse is passed through it. In nonslapper types, the exploding conductor starts a chemical detonation in a contacting highexplosive material such as PETN (pentaerythritoltetranitrate). In slapper detonators, the explosive vaporization of the electrical conductor drives a flyer or slapper across a gap, and the impact of the slapper on an explosive starts a chemical detonation. The slapper in some designs is driven by magnetic force. The term exploding foil detonator may refer to either an EB or a slapper-type detonator. Also, the word initiator is sometimes used in place of the word detonator. |
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3A233 |
Mass spectrometers, other than those specified in 0B002.g., capable of measuring ions of 230 atomic mass units or greater and having a resolution of better than 2 parts in 230, as follows, and ion sources therefor:
Technical Notes:
|
3.B.6. |
Mass spectrometers capable of measuring ions of 230 atomic mass units or greater and having a resolution of better than 2 parts in 230, as follows, and ion sources therefor:
|
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3A234 |
Striplines to provide low inductance path to detonators with the following characteristics:
|
6.A.6. |
Striplines to provide low inductance path to detonators with the following characteristics:
|
3D Software
The corresponding systems, equipment and components as identified in Council Regulation (EC) No 428/2009 of 5 May 2009 setting up a Community regime for the control of exports, transfer, brokering and transit of dual-use items |
Nuclear Suppliers Group's control list as in INFCIRC/254/Rev.9/Part 2 |
||
3D002 |
“Software” specially designed for the “use” of equipment specified in 3B001.a. to f., 3B002 or 3A225 |
3.D.1. |
“Software” specially designed for the “use” of equipment specified in Items 3.A.1., 3.B.3. or 3.B.4. |
3D225 |
“Software” specially designed to enhance or release the performance of frequency changers or generators to meet the characteristics of 3A225. |
3.D.3. |
“Software” specially designed to enhance or release the performance characteristics of equipment controlled in Item 3.A.1. |
3E Technology
The corresponding systems, equipment and components as identified in Council Regulation (EC) No 428/2009 of 5 May 2009 setting up a Community regime for the control of exports, transfer, brokering and transit of dual-use items |
Nuclear Suppliers Group's control list as in INFCIRC/254/Rev.9/Part 2 |
||||||||||
3E001 |
“Technology” according to the General Technology Note for the “development” or “production” of equipment or materials specified in 3A, 3B or 3C;
|
3.E.1 |
“Technology” according to the Technology Controls for the “development”, “production” or “use” of equipment, material or “software” specified in 3.A. through 3.D. |
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3E201 |
“Technology” according to the General Technology Note for the “use” of equipment specified in 3A001.e.2., 3A001.e.3., 3A001.g., 3A201, 3A225 to 3A234. |
3.E.1 |
“Technology” according to the Technology Controls for the “development”, “production” or “use” of equipment, material or “software” specified in 3.A. through 3.D. |
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3E225 |
“Technology”, in the form of codes or keys, to enhance or release the performance of frequency changers or generators to meet the characteristics of 3A225. |
3.E.1 |
“Technology” according to the Technology Controls for the “development”, “production” or “use” of equipment, material or “software” specified in 3.A. through 3.D. |
CATEGORY 6 — SENSORS AND LASERS
6A Systems, Equipment and Components
The corresponding systems, equipment and components as identified in Council Regulation (EC) No 428/2009 of 5 May 2009 setting up a Community regime for the control of exports, transfer, brokering and transit of dual-use items |
Nuclear Suppliers Group's control list as in INFCIRC/254/Rev.9/Part 2 |
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6A005 |
“Lasers”, other than those specified in 0B001.g.5. or 0B001.h.6., components and optical equipment, as follows:
Technical Note: In 6A005 ‘Wall-plug efficiency’ is defined as the ratio of “laser” output power (or “average output power”) to total electrical input power required to operate the “laser”, including the power supply/conditioning and thermal conditioning/heat exchanger.
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3.A.2 |
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3.A.2 |
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3.A.2 |
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6A202 |
Photomultiplier tubes having both of the following characteristics:
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5.A.1. |
Photomultiplier tubes having both of the following characteristics:
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6A203 |
Cameras and components, other than those specified in 6A003, as follows:
Note: 6A203.a. to 6A203.c. does not control cameras or imaging devices if they have hardware, “software” or “technology” constraints that limit the performance to less than that specified above, provided they meet any of the following:
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5.B.3. |
High-speed cameras and imaging devices and components therefor, as follows:
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6A203 |
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5.B.3.a |
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6A203 |
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5.B.3.b |
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6A203 |
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5.B.3.c |
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6A203 |
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1.A.2. |
Radiation-hardened TV cameras, or lenses therefor, specially designed or rated as radiation hardened to withstand a total radiation dose greater than 5 × 104 Gy (silicon) without operational degradation. Technical Note: The term Gy (silicon) refers to the energy in Joules per kilogram absorbed by an unshielded silicon sample when exposed to ionizing radiation. |
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6A205 |
“Lasers”, “laser” amplifiers and oscillators, other than those specified in 0B001.g.5., 0B001.h.6. and 6A005; as follows:
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3.A.2. |
Lasers, laser amplifiers and oscillators as follows:
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6A205 |
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3.A.2.b |
Argon ion lasers having both of the following characteristics:
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6A205 |
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3.A.2.d |
Tunable pulsed single-mode dye laser oscillators having all of the following characteristics:
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6A205 |
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3.A.2.e |
Tunable pulsed dye laser amplifiers and oscillators having all of the following characteristics:
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6A205 |
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3.A.2.g |
Pulsed carbon dioxide lasers having all of the following characteristics:
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6A205 |
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3.A.2.i. |
Para-hydrogen Raman shifters designed to operate at 16 mm output wavelength and at a repetition rate greater than 250 Hz. |
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6A205 |
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3.A.2.c. |
Neodymium-doped (other than glass) lasers with an output wavelength between 1 000 and 1 100 nm having either of the following:
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6A205 |
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3.A.2.j |
Pulsed carbon monoxide lasers having all of the following characteristics:
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6A225 |
Velocity interferometers for measuring velocities exceeding 1 km/s during time intervals of less than 10 microseconds.
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5.B.5.a |
Specialized instrumentation for hydrodynamic experiments, as follows:
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6A226 |
Pressure sensors, as follows:
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5.B.5.b. |
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5.B.5.c. |
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6D Software
The corresponding systems, equipment and components as identified in Council Regulation (EC) No 428/2009 of 5 May 2009 setting up a Community regime for the control of exports, transfer, brokering and transit of dual-use items |
Nuclear Suppliers Group's control list as in INFCIRC/254/Rev.9/Part 2 |
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6D203 |
“Software” specially designed to enhance or release the performance of cameras or imaging devices to meet the characteristics of 6A203.a. to 6A203.c. |
5.D.2. |
“Software” or encryption keys/codes specially designed to enhance or release the performance characteristics of equipment controlled in Item 5.B.3. |
6E Technology
The corresponding systems, equipment and components as identified in Council Regulation (EC) No 428/2009 of 5 May 2009 setting up a Community regime for the control of exports, transfer, brokering and transit of dual-use items |
Nuclear Suppliers Group's control list as in INFCIRC/254/Rev.9/Part 2 |
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6E201 |
“Technology” according to the General Technology Note for the “use” of equipment specified in 6A003, 6A005.a.2., 6A005.b.2., 6A005.b.3., 6A005.b.4., 6A005.b.6., 6A005.c.2., 6A005.d.3.c., 6A005.d.4.c., 6A202, 6A203, 6A205, 6A225 or 6A226. |
5.D.1. |
“Technology” according to the Technology Controls for the “development”, “production” or “use” of equipment, material or “software” specified in 5.A. through 5.D. |
6E203 |
“Technology”, in the form of codes or keys, to enhance or release the performance of cameras or imaging devices to meet the characteristics of 6A203a. to 6A203.c. |
5.D.1. |
“Technology” according to the Technology Controls for the “development”, “production” or “use” of equipment, material or “software” specified in 5.A. through 5.D.’ |
(1) Item codes marked with a “TLB” refer to items listed in Annex B of the NSG Part 1 Trigger List. Item codes marked with “TLA” refer to items listed in Annex A of NSG Part 1 Trigger List. Item codes marked with neither “TLB” nor “TLA” refer to items listed in the NSG Dual Use List, referenced in the Categories 1, 2 and 6.
(2) Manufacturers calculating positioning accuracy in accordance with ISO 230/2 (1997) or (2006) should consult the competent authorities of the Member State in which they are established.
ANNEX II
‘ANNEX III
CATEGORY 1 — SPECIAL MATERIALS AND RELATED EQUIPMENT
1A Systems, Equipment and Components
The corresponding systems, equipment and components as identified in Council Regulation (EC) No 428/2009 of 5 May 2009 setting up a Community regime for the control of exports, transfer, brokering and transit of dual-use items |
Missile Technology Control Regime (M.TCR): Equipment, software and technology annex |
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1A002 |
“Composite” structures or laminates, having any of the following:
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M6A1 |
Composite structures, laminates, and manufactures thereof, specially designed for use in the systems specified in 1.A., 19.A.1. or 19.A.2. and the subsystems specified in 2.A. or 20.A. |
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1A102 |
Resaturated pyrolized carbon-carbon components designed for space launch vehicles specified in 9A004 or sounding rockets specified in 9A104. |
M6A2 |
Resaturated pyrolised (i.e. carbon-carbon) components having all of the following: a. Designed for rocket systems; and b. Usable in the systems specified in 1.A. or 19.A.1. |
1B Test, Inspection and Production Equipment
The corresponding systems, equipment and components as identified in Council Regulation (EC) No 428/2009 of 5 May 2009 setting up a Community regime for the control of exports, transfer, brokering and transit of dual-use items |
Missile Technology Control Regime (M.TCR): Equipment, software and technology annex |
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1B001 |
Equipment for the production or inspection of “composite” structures or laminates specified in 1A002 or “fibrous or filamentary materials” specified in 1C010, as follows, and specially designed components and accessories therefor:
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M6B1a |
Filament winding machines or ‘fibre/tow-placement machines’, of which the motions for positioning, wrapping and winding fibres can be coordinated and programmed in three or more axes, designed to fabricate composite structures or laminates from fibrous or filamentary materials, and co-ordinating and programming controls |
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M6B1b |
‘Tape-laying machines’ of which the motions for positioning and laying tape can be co-ordinated and programmed in two or more axes, designed for the manufacture of composite airframes and missile structures;
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M6B1c |
Multi-directional, multi-dimensional weaving machines or interlacing machines, including adapters and modification kits for weaving, interlacing or braiding fibres to manufacture composite structures;
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Equipment designed or modified for the production of fibrous or filamentary materials as follows: |
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M6B1d1 |
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M6B1d2 |
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M6B1d3 |
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M6B1e |
Equipment designed or modified for special fibre surface treatment or for producing prepregs and preforms, including rollers, tension stretchers, coating equipment, cutting equipment and clicker dies.
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1B002 |
Equipment for producing metal alloys, metal alloy powder or alloyed materials, specially designed to avoid contamination and specially designed for use in one of the processes specified in 1C002.c.2.
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M4B3d |
Metal powder “production equipment” usable for the “production”, in a controlled environment, of spherical, spheroidal or atomised materials specified in 4.C.2.c., 4.C.2.d. or 4.C.2.e. Note: 4.B.3.d. includes: a. Plasma generators (high frequency arc-jet) usable for obtaining sputtered or spherical metallic powders with organization of the process in an argon-water environment; b. Electroburst equipment usable for obtaining sputtered or spherical metallic powders with organization of the process in an argon-water environment; c. Equipment usable for the “production” of spherical aluminium powders by powdering a melt in an inert medium (e.g. nitrogen). Notes:
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1B101 |
Equipment, other than that specified in 1B001, for the “production” of structural composites as follows; and specially designed components and accessories therefor:
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M6B1a |
Filament winding machines or ‘fibre/tow-placement machines’, of which the motions for positioning, wrapping and winding fibres can be coordinated and programmed in three or more axes, designed to fabricate composite structures or laminates from fibrous or filamentary materials, and co-ordinating and programming controls; |
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M6B1b |
‘Tape-laying machines’ of which the motions for positioning and laying tape can be co-ordinated and programmed in two or more axes, designed for the manufacture of composite airframes and missile structures; Note: For the purposes of 6.B.1.a. and 6.B.1.b., the following definitions apply:
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M6B1d |
Equipment designed or modified for the production of fibrous or filamentary materials as follows:
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M6B1e |
Equipment designed or modified for special fibre surface treatment or for producing prepregs and preforms, including rollers, tension stretchers, coating equipment, cutting equipment and clicker dies.
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1B102 |
Metal powder “production equipment”, other than that specified in 1B002, and components as follows:
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M4B3d |
Metal powder “production equipment” usable for the “production”, in a controlled environment, of spherical, spheroidal or atomised materials specified in 4.C.2.c., 4.C.2.d. or 4.C.2.e.
Notes:
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1B115 |
Equipment, other than that specified in 1B002 or 1B102, for the production of propellant and propellant constituents, as follows, and specially designed components therefor: |
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M4B1 |
“Production equipment”, and specially designed components therefor, for the “production”, handling or acceptance testing of liquid propellants or propellant constituents specified in 4.C. |
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M4B2 |
“Production equipment”, other than that described in 4.B.3., and specially designed components therefor, for the production, handling, mixing, curing, casting, pressing, machining, extruding or acceptance testing of solid propellants or propellant constituents specified in 4.C. |
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1B116 |
Specially designed nozzles for producing pyrolitically derived materials formed on a mould, mandrel or other substrate from precursor gases which decompose in the 1 573 K (1 300 °C) to 3 173 K (2 900 °C) temperature range at pressures of 130 Pa to 20 kPa. |
M6B2 |
Nozzles specially designed for the processes referred to in 6.E.3. |
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1B117 |
Batch mixers with provision for mixing under vacuum in the range of zero to 13,326 kPa and with temperature control capability of the mixing chamber and having all of the following, and specially designed components therefor:
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M4B3a |
Batch mixers with provision for mixing under vacuum in the range of zero to 13,326 kPa and with temperature control capability of the mixing chamber and having all of the following:
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1B118 |
Continuous mixers with provision for mixing under vacuum in the range of zero to 13,326 kPa and with a temperature control capability of the mixing chamber having any of the following, and specially designed components therefor:
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M4B3b |
Continuous mixers with provision for mixing under vacuum in the range of zero to 13,326 kPa and with a temperature control capability of the mixing chamber having any of the following:
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1B119 |
Fluid energy mills usable for grinding or milling substances specified in 1C011.a., 1C011.b., 1C111 or in the Military Goods Controls, and specially designed components therefor. |
M4B3c |
Fluid energy mills usable for grinding or milling substances specified in 4.C |
1C Materials
The corresponding systems, equipment and components as identified in Council Regulation (EC) No 428/2009 of 5 May 2009 setting up a Community regime for the control of exports, transfer, brokering and transit of dual-use items |
Missile Technology Control Regime (M.TCR): Equipment, software and technology annex |
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1C001 |
Materials specially designed for use as absorbers of electromagnetic waves, or intrinsically conductive polymers, as follows:
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M17C1 |
Materials for reduced observables such as radar reflectivity, ultraviolet/infrared signatures and acoustic signatures (i.e. stealth technology), for applications usable for the systems specified in 1.A. or 19.A. or the subsystems specified in 2.A. Notes:
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1C007 |
Ceramic powders, non-“composite” ceramic materials, ceramic-“matrix”“composite” materials and precursor materials, as follows:
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M6C5 |
Ceramic composite materials (dielectric constant less than 6 at any frequency from 100 MHz to 100 GHz) for use in missile radomes usable in systems specified in 1.A. or 19.A.1. |
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M6C6 |
Silicon-carbide materials as follows:
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1C010 |
“Fibrous or filamentary materials”, as follows:
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M6C1 |
Resin impregnated fibre prepregs and metal coated fibre preforms, for the goods specified in 6.A.1., made either with organic matrix or metal matrix utilising fibrous or filamentary reinforcements having a specific tensile strength greater than 7,62 × 104 m and a specific modulus greater than 3,18 × 106 m.
Technical Notes:
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1C011 |
Metals and compounds, as follows:
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M4C2d |
Metal powders of any of the following: zirconium (CAS 7440-67-7), beryllium (CAS 7440-41-7), magnesium (CAS 7439-95-4) or alloys of these, if at least 90 % of the total particles by particle volume or weight are made up of particles of less than 60 μm (determined by measurement techniques such as using a sieve, laser diffraction or optical scanning), whether spherical, atomised, spheroidal, flaked or ground, consisting of 97 % by weight or more of any of the above mentioned metals;
Technical Note: The natural content of hafnium (CAS 7440-58-6) in the zirconium (typically 2 % to 7 %) is counted with the zirconium. |
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M4C2e |
Metal powders of either boron (CAS 7440-42-8) or boron alloys with a boron content of 85 % or more by weight, if at least 90 % of the total particles by particle volume or weight are made up of particles of less than 60 μm (determined by measurement techniques such as using a sieve, laser diffraction or optical scanning), whether spherical, atomised, spheroidal, flaked or ground;
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1C101 |
Materials and devices for reduced observables such as radar reflectivity, ultraviolet/infrared signatures and acoustic signatures, other than those specified in 1C001, usable in ‘missiles’, “missile” subsystems or unmanned aerial vehicles specified in 9A012 or 9A112.a.
Technical Note: In 1C101 ‘missile’ means complete rocket systems and unmanned aerial vehicle systems capable of a range exceeding 300 km. |
M17A1 |
Devices for reduced observables such as radar reflectivity, ultraviolet/infrared signatures and acoustic signatures (i.e. stealth technology), for applications usable for the systems specified in 1.A. or 19.A. or the subsystems specified in 2.A. or 20.A. |
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M17C1 |
Materials for reduced observables such as radar reflectivity, ultraviolet/infrared signatures and acoustic signatures (i.e. stealth technology), for applications usable for the systems specified in 1.A. or 19.A. or the subsystems specified in 2.A. Notes:
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1C102 |
Resaturated pyrolized carbon-carbon materials designed for space launch vehicles specified in 9A004 or sounding rockets specified in 9A104. |
M6C2 |
Resaturated pyrolised (i.e. carbon-carbon) materials having all of the following: a. Designed for rocket systems; and b. Usable in the systems specified in 1.A. or 19.A.1. |
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1C107 |
Graphite and ceramic materials, other than those specified in 1C007, as follows: |
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M6C3 |
Fine grain graphites with a bulk density of at least 1,72 g/cc measured at 15 °C and having a grain size of 100 × 10-6 m (100 μm) or less, usable for rocket nozzles and re-entry vehicle nose tips, which can be machined to any of the following products:
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M6C4 |
Pyrolytic or fibrous reinforced graphites usable for rocket nozzles and reentry vehicle nose tips usable in systems specified in 1.A. or 19.A.1. |
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M6C5 |
Ceramic composite materials (dielectric constant less than 6 at any frequency from 100 MHz to 100 GHz) for use in missile radomes usable in systems specified in 1.A. or 19.A.1. |
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M6C6a |
Bulk machinable silicon-carbide reinforced unfired ceramic usable for nose tips usable in systems specified in 1.A. or 19.A.1.; |
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M6C6b |
Reinforced silicon-carbide ceramic composites usable for nose tips, re-entry vehicles, nozzle flaps, usable in systems specified in 1.A. or 19.A.1. |
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1C111 |
Propellants and constituent chemicals for propellants, other than those specified in 1C011, as follows:
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M4C2c |
Spherical or spheroidal aluminium powder (CAS 7429-90-5) in particle size of less than 200 × 10-6 m (200 μm) and an aluminium content of 97 % by weight or more, if at least 10 % of the total weight is made up of particles of less than 63 μm, according to ISO 2591-1:1988 or national equivalents; Technical Note: A particle size of 63 μm (ISO R-565) corresponds to 250 mesh (Tyler) or 230 mesh (ASTM standard E-11). |
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M4C2d |
Metal powders of any of the following: zirconium (CAS 7440-67-7), beryllium (CAS 7440-41-7), magnesium (CAS 7439-95-4) or alloys of these, if at least 90 % of the total particles by particle volume or weight are made up of particles of less than 60 μm (determined by measurement techniques such as using a sieve, laser diffraction or optical scanning), whether spherical, atomised, spheroidal, flaked or ground, consisting of 97 % by weight or more of any of the above mentioned metals;
Technical Note: The natural content of hafnium (CAS 7440-58-6) in the zirconium (typically 2 % to 7 %) is counted with the zirconium. |
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M4C2e |
Metal powders of either boron (CAS 7440-42-8) or boron alloys with a boron content of 85 % or more by weight, if at least 90 % of the total particles by particle volume or weight are made up of particles of less than 60 μm (determined by measurement techniques such as using a sieve, laser diffraction or optical scanning), whether spherical, atomised, spheroidal, flaked or ground
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M4C4a |
Oxidiser substances usable in liquid propellant rocket engines as follows:
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M4C2b |
Hydrazine derivatives as follows:
Technical note: 3,6-dihydrazino tetrazine nitrate is also referred to as 1,4-dihydrazine nitrate. |
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M4C2f |
High energy density materials, usable in the systems specified in 1.A. or 19.A., as follows:
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M4C2g |
Hydrazine replacement fuels as follows: 1. 2-Dimethylaminoethylazide (DMAZ) (CAS 86147-04-8). |
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M4C5 |
Polymeric substances, as follows:
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M4C6c1 |
Carboranes, decaboranes, pentaboranes and derivatives thereof |
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M4C6d1 |
Triethylene glycol dinitrate (TEGDN) (CAS 111-22-8); |
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M4C6e1 |
2-Nitrodiphenylamine (CAS 119-75-5); |
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M4C6d2 |
Trimethylolethane trinitrate (TMETN) (CAS 3032-55-1); |
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M4C6d4 |
Diethylene glycol dinitrate (DEGDN) (CAS 693-21-0) |
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M4C6c2 |
Ferrocene derivatives, as follows:
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M4C6d5 |
4,5 diazidomethyl-2-methyl-1,2,3-triazole (iso- DAMTR); |
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1C116 |
Maraging steels, useable in ‘missiles’, having all of the following:
|
M6C8 |
Maraging steels, usable in the systems specified in 1.A. or 19.A.1., having all of the following:
Technical Note: Maraging steels are iron alloys:
|
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1C117 |
Materials for the fabrication of ‘missiles’ components as follows:
Technical Note: In 1C117 ‘missile’ means complete rocket systems and unmanned aerial vehicle systems capable of a range exceeding 300 km. |
M6C7 |
Materials for the fabrication of missile components in the systems specified in 1.A., 19.A.1. or 19.A.2, as follows:.
|
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1C118 |
Titanium-stabilised duplex stainless steel (Ti-DSS) having all of the following:
|
M6C9 |
Titanium-stabilized duplex stainless steel (Ti-DSS) usable in the systems specified in 1.A. or 19.A.1. and having all of the following:
|
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1C238 |
Chlorine trifluoride (ClF3). |
M4C4a6 |
Compounds composed of fluorine and one or more of other halogens, oxygen or nitrogen;
|
1D Software
The corresponding systems, equipment and components as identified in Council Regulation (EC) No 428/2009 of 5 May 2009 setting up a Community regime for the control of exports, transfer, brokering and transit of dual-use items |
Missile Technology Control Regime (M.TCR): Equipment, software and technology annex |
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1D001 |
“Software” specially designed or modified for the “development”, “production” or “use” of equipment specified in 1B001 to 1B003. |
M6D1 |
“Software” specially designed or modified for the operation or maintenance of equipment specified in 6.B.1. |
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1D101 |
“Software” specially designed or modified for the operation or maintenance of goods specified in1B101, 1B102, 1B115, 1B117, 1B118 or 1B119. |
M4D1 |
“Software” specially designed or modified for the operation or maintenance of equipment specified in 4.B. for the “production” and handling of materials specified in 4.C. |
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M6D1 |
“Software” specially designed or modified for the operation or maintenance of equipment specified in 6.B.1. |
||||
1D103 |
“Software” specially designed for analysis of reduced observables such as radar reflectivity, ultraviolet/infrared signatures and acoustic signatures. |
M17D1 |
“Software” specially designed for reduced observables such as radar reflectivity, ultraviolet/infrared signatures and acoustic signatures (i.e. stealth technology), for applications usable for the systems specified in 1.A. or 19.A. or the subsystems specified in 2.A.
|
1E Technology
The corresponding systems, equipment and components as identified in Council Regulation (EC) No 428/2009 of 5 May 2009 setting up a Community regime for the control of exports, transfer, brokering and transit of dual-use items |
Missile Technology Control Regime (M.TCR): Equipment, software and technology annex |
||||
1E001 |
“Technology” according to the General Technology Note for the “development” or “production” of equipment or materials specified in 1A001.b., 1A001.c., 1A002 to 1A005, 1A006.b., 1A007, 1B or 1C. |
M |
“Technology”, in accordance with the General Technology Note, for the “development”, “production” or “use” of equipment or “software” specified in 1.A., 1.B., or 1.D. |
||
1E101 |
“Technology” according to the General Technology Note for the “use” of goods specified in 1A102, 1B001, 1B101, 1B102, 1B115 to 1B119, 1C001, 1C101, 1C107, 1C111 to 1C118, 1D101 or 1D103. |
M |
“Technology”, in accordance with the General Technology Note, for the “development”, “production” or “use” of equipment or “software” specified in 1.A., 1.B., or 1.D. |
||
1E102 |
“Technology” according to the General Technology Note for the “development” of “software” specified in 1D001, 1D101 or 1D103. |
M6E1 |
“Technology”, in accordance with the General Technology Note, for the “development”, “production” or “use” of equipment, materials or “software” specified in 6.A., 6.B., 6.C. or 6.D. |
||
M17E1 |
“Technology”, in accordance with the General Technology Note, for the “development”, “production” or “use” of equipment, materials or “software” specified in 17.A., 17.B., 17.C. or 17.D.
|
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1E103 |
[M6E2]“Technology” for the regulation of temperature, pressure or atmosphere in autoclaves or hydroclaves, when used for the “production” of “composites” or partially processed “composites”. |
M6E2 |
“Technical data” (including processing conditions) and procedures for the regulation of temperature, pressures or atmosphere in autoclaves or hydroclaves when used for the production of composites or partially processed composites, usable for equipment or materials specified in 6.A. or 6.C |
||
1E104 |
“Technology” relating to the “production” of pyrolytically derived materials formed on a mould, mandrel or other substrate from precursor gases which decompose in the 1 573 K (1 300 °C) to 3 173 K (2 900 °C) temperature range at pressures of 130 Pa to 20 kPa.
|
M6E1 |
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CATEGORY 2 — MATERRIALS PROCESSING
The corresponding systems, equipment and components as identified in Council Regulation (EC) No 428/2009 of 5 May 2009 setting up a Community regime for the control of exports, transfer, brokering and transit of dual-use items |
Missile Technology Control Regime (M.TCR): Equipment, software and technology annex |
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2A001 |
Anti-friction bearings and bearing systems, as follows, and components therefor:
|
M3A7 |
Radial ball bearings having all tolerances specified in accordance with ISO 492 Tolerance Class 2 (or ANSI/ABMA Std 20 Tolerance Class ABEC-9 or other national equivalents), or better and having all the following characteristics:
|
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2A101 |
Radial ball bearings, other than those specified in 2A001, having all tolerances specified in accordance with ISO 492 Tolerance Class 2 (or ANSI/ABMA Std 20 Tolerance Class ABEC-9 or other national equivalents), or better and having all the following characteristics:
|
M3A7 |
Radial ball bearings having all tolerances specified in accordance with ISO 492 Tolerance Class 2 (or ANSI/ABMA Std 20 Tolerance Class ABEC-9 or other national equivalents), or better and having all the following characteristics:
|
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2B004 |
Hot “isostatic presses” having all of the following, and specially designed components and accessories therefor:
Technical Note: The inside chamber dimension is that of the chamber in which both the working temperature and the working pressure are achieved and does not include fixtures. That dimension will be the smaller of either the inside diameter of the pressure chamber or the inside diameter of the insulated furnace chamber, depending on which of the two chambers is located inside the other.
|
M6B3 |
Isostatic presses having all of the following characteristics:
|
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2B009 |
Spin-forming machines and flow-forming machines, which, according to the manufacturer's technical specification, can be equipped with “numerical control” units or a computer control and having all of the following:
Technical Note: For the purpose of 2B009, machines combining the function of spin-forming and flow-forming are regarded as flow-forming machines. |
M3B3 |
Flow-forming machines, and specially designed components therefor, which:
Technical Note: Machines combining the function of spin-forming and flow-forming are, for the purpose of this item, regarded as flow-forming machines. |
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2B104 |
“Isostatic presses”, other than those specified in 2B004, having all of the following:
|
M6B3 |
Isostatic presses having all of the following characteristics:
|
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2B105 |
Chemical vapour deposition (CVD) furnaces, other than those specified in 2B005.a., designed or modified for the densification of carbon-carbon composites. |
M6B4 |
Chemical vapour deposition furnaces designed or modified for the densification of carbon-carbon composites. |
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2B109 |
Flow-forming machines, other than those specified in 2B009, and specially designed components as follows:
Technical Note: Machines combining the function of spin-forming and flow-forming are for the purpose of 2B109 regarded as flow-forming machines. |
M3B3 |
Flow-forming machines, and specially designed components therefor, which:
Technical Note: Machines combining the function of spin-forming and flow-forming are, for the purpose of this item, regarded as flow-forming machines. |
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2B116 |
Vibration test systems, equipment and components therefor, as follows:
Technical Note: In 2B116, ‘bare table’ means a flat table, or surface, with no fixture or fittings. |
M15B1 |
Vibration test equipment, usable for the systems specified in 1.A., 19.A.1. or 19.A.2. or the subsystems specified in 2.A. or 20.A., and components therefor, as follows:
Technical Note: Vibration test systems incorporating a digital controller are those systems, the functions of which are, partly or entirely, automatically controlled by stored and digitally coded electrical signals. |
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2B117 |
Equipment and process controls, other than those specified in 2B004, 2B005.a., 2B104 or 2B105, designed or modified for densification and pyrolysis of structural composite rocket nozzles and reentry vehicle nose tips. |
M6B5 |
Equipment and process controls, other than those specified in 6.B.3. or 6.B.4., designed or modified for densification and pyrolysis of structural composite rocket nozzles and re-entry vehicle nose tips. |
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2B119 |
Balancing machines and related equipment, as follows:
|
M9B2a |
Equipment as follows:
|
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M9B2b |
Indicator heads (sometimes known as balancing instrumentation) designed or modified for use with machines specified in 9.B.2.a.; |
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2B120 |
Motion simulators or rate tables having all of the following characteristics:
|
M9B2c |
Motion simulators/rate tables (equipment capable of simulating motion) having all of the following characteristics:
|
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2B121 |
Positioning tables (equipment capable of precise rotary positioning in any axes), other than those specified in 2B120, having all the following characteristics:
|
M9B2d |
Positioning tables (equipment capable of precise rotary positioning in any axes) having the following characteristics:
|
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2B122 |
Centrifuges capable of imparting accelerations above 100 g and designed or modified to incorporate slip rings or integrated non-contact devices capable of transferring electrical power, signal information, or both.
|
M9B2e |
Centrifuges capable of imparting accelerations above 100 g and designed or modified to incorporate sliprings or integrated non-contact devices capable of transferring electrical power, signal information, or both |
2D Software
The corresponding systems, equipment and components as identified in Council Regulation (EC) No 428/2009 of 5 May 2009 setting up a Community regime for the control of exports, transfer, brokering and transit of dual-use items |
Missile Technology Control Regime (M.TCR): Equipment, software and technology annex |
||||||||
2D001 |
“Software”, other than that specified in 2D002, as follows:
|
M3D |
SOFTWARE |
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2D101 |
“Software” specially designed or modified for the “use” of equipment specified in 2B104, 2B105, 2B109, 2B116, 2B117 or 2B119 to 2B122.
|
M3D1 |
“Software” specially designed or modified for the “use” of “production facilities” and flow-forming machines specified in 3.B.1. or 3.B.3. |
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M6D2 |
“Software” specially designed or modified for the equipment specified in 6.B.3., 6.B.4. or 6.B.5. |
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M15D1 |
“Software” specially designed or modified for the “use” of equipment specified in 15.B. usable for testing systems specified in 1.A., 19.A.1. or 19.A.2. or subsystems specified in 2.A. or 20.A. |
2E Technology
The corresponding systems, equipment and components as identified in Council Regulation (EC) No 428/2009 of 5 May 2009 setting up a Community regime for the control of exports, transfer, brokering and transit of dual-use items |
Missile Technology Control Regime (M.TCR): Equipment, software and technology annex |
||||
2E001 |
“Technology” according to the General Technology Note for the “development” of equipment or “software” specified in 2A, 2B or 2D.
|
M |
Means specific information which is required for the “development”, “production” or “use” of a product. The information may take the form of “technical data” or “technical assistance”. |
||
2E002 |
“Technology” according to the General Technology Note for the “production” of equipment specified in 2A or 2B. |
M |
Means specific information which is required for the “development”, “production” or “use” of a product. The information may take the form of “technical data” or “technical assistance”. |
||
2E101 |
“Technology” according to the General Technology Note for the “use” of equipment or “software” specified in 2B004, 2B009, 2B104, 2B109, 2B116, 2B119 to 2B122 or 2D101. |
M |
Means specific information which is required for the “development”, “production” or “use” of a product. The information may take the form of “technical data” or “technical assistance”. |
CATEGORY 3 — ELECTRONICS
3A Systems, Equipment and Components
The corresponding systems, equipment and components as identified in Council Regulation (EC) No 428/2009 of 5 May 2009 setting up a Community regime for the control of exports, transfer, brokering and transit of dual-use items |
Missile Technology Control Regime (M.TCR): Equipment, software and technology annex |
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3A001 |
Electronic components and specially designed components therefor, as follows:
|
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M18A1 |
“Radiation Hardened”“microcircuits” usable in protecting rocket systems and unmanned aerial vehicles against nuclear effects (e.g. Electromagnetic Pulse (EMP), X-rays, combined blast and thermal effects), and usable for the systems specified in 1.A. |
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M18A2 |
‘Detectors’ specially designed or modified to protect rocket systems and unmanned aerial vehicles against nuclear effects (e.g. Electromagnetic Pulse (EMP), X-rays, combined blast and thermal effects), and usable for the systems specified in 1.A. Technical Note: A ‘detector’ is defined as a mechanical, electrical, optical or chemical device that automatically identifies and records, or registers a stimulus such as an environmental change in pressure or temperature, an electrical or electromagnetic signal or radiation from a radioactive material. This includes devices that sense by one time operation or failure. |
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3A101 |
Electronic equipment, devices and components, other than those specified in 3A001, as follows:
|
M14A1 |
Analogue-to-digital converters, usable in the systems specified in 1.A., having any of the following characteristics:
|
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M14A1b1 |
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M14A1b2 |
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M15B5 |
Accelerators capable of delivering electromagnetic radiation produced by bremsstrahlung from accelerated electrons of 2 MeV or greater, and equipment containing those accelerators, usable for the systems specified in 1.A., 19.A.1. or 19.A.2. or the subsystems specified in 2.A. or 20.A.
Technical Note: In Item 15.B. ‘bare table’ means a flat table, or surface, with no fixture or fittings. |
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3A102 |
‘Thermal batteries’ designed or modified for ‘missiles’. Technical Notes:
|
M12A6 |
Thermal batteries designed or modified for the systems specified in 1.A., 19.A.1. or 19.A.2.
Technical Note: Thermal batteries are single use batteries that contain a solid non-conducting inorganic salt as the electrolyte. These batteries incorporate a pyrolytic material that, when ignited, melts the electrolyte and activates the battery. |
3D Software
The corresponding systems, equipment and components as identified in Council Regulation (EC) No 428/2009 of 5 May 2009 setting up a Community regime for the control of exports, transfer, brokering and transit of dual-use items |
Missile Technology Control Regime (M.TCR): Equipment, software and technology annex |
||
3D101 |
“Software” specially designed or modified for the “use” of equipment specified in 3A101.b. |
M15D1 |
“Software” specially designed or modified for the “use” of equipment specified in 3A101.b. |
3E Technology
The corresponding systems, equipment and components as identified in Council Regulation (EC) No 428/2009 of 5 May 2009 setting up a Community regime for the control of exports, transfer, brokering and transit of dual-use items |
Missile Technology Control Regime (M.TCR): Equipment, software and technology annex |
||||||||||
3E001 |
“Technology” according to the General Technology Note for the “development” or “production” of equipment or materials specified in 3A, 3B or 3C;
|
M |
Means specific information which is required for the “development”, “production” or “use” of a product. The information may take the form of “technical data” or “technical assistance”. |
||||||||
3E101 |
“Technology” according to the General Technology Note for the “use” of equipment or “software” specified in 3A001.a.1. or 2., 3A101, 3A102 or 3D101. |
M |
Means specific information which is required for the “development”, “production” or “use” of a product. The information may take the form of “technical data” or “technical assistance”. |
||||||||
3E102 |
“Technology” according to the General Technology Note for the “development” of “software” specified in 3D101. |
M15E1 |
“Technology”, in accordance with the General Technology Note, for the “development”, “production” or “use” of equipment or “software” specified in 15.B. or 15.D. |
CATEGORY 4 — COMPUTERS
4A Systems, Equipment and Components
The corresponding systems, equipment and components as identified in Council Regulation (EC) No 428/2009 of 5 May 2009 setting up a Community regime for the control of exports, transfer, brokering and transit of dual-use items |
Missile Technology Control Regime (M.TCR): Equipment, software and technology annex |
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4A001 |
Electronic computers and related equipment, having any of the following and “electronic assemblies” and specially designed components therefor:
|
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|
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M13A1 |
Analogue computers, digital computers or digital differential analysers, designed or modified for use in the systems specified in 1.A., having any of the following characteristics:
|
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4A003 |
“Digital computers”, “electronic assemblies”, and related equipment therefor, as follows and specially designed components therefor:
|
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M14A1b2 |
Electrical input type analogue-to-digital converter printed circuit boards or modules, having all of the following characteristics:
|
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4A101 |
Analogue computers, “digital computers” or digital differential analysers, other than those specified in 4A001.a.1., which are ruggedized and designed or modified for use in space launch vehicles specified in 9A004 or sounding rockets specified in 9A104. |
M13A1b |
Designed as ruggedised or “radiation hardened”. |
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4A102 |
“Hybrid computers” specially designed for modelling, simulation or design integration of space launch vehicles specified in 9A004 or sounding rockets specified in 9A104.
|
M16A1 |
Specially designed hybrid (combined analogue/digital) computers for modelling, simulation or design integration of systems specified in 1.A. or the subsystems specified in 2.A.
|
4E Technology
The corresponding systems, equipment and components as identified in Council Regulation (EC) No 428/2009 of 5 May 2009 setting up a Community regime for the control of exports, transfer, brokering and transit of dual-use items |
Missile Technology Control Regime (M.TCR): Equipment, software and technology annex |
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4E001 |
|
M |
Means specific information which is required for the “development”, “production” or “use” of a product. The information may take the form of “technical data” or “technical assistance”. |
CATEGORY 5 — TELECOMMUNICATIONS AND “INFORMATION SECURITY”
Part 1 — Telecommunications
5A1 Systems, Equipment and Components
The corresponding systems, equipment and components as identified in Council Regulation (EC) No 428/2009 of 5 May 2009 setting up a Community regime for the control of exports, transfer, brokering and transit of dual-use items |
Missile Technology Control Regime (M.TCR): Equipment, software and technology annex |
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5A101 |
Telemetry and telecontrol equipment, including ground equipment, designed or modified for ‘missiles’. Technical Note: In 5A101 ‘missile’ means complete rocket systems and unmanned aerial vehicle systems capable of a range exceeding 300 km.
|
M12A4 |
Telemetry and telecontrol equipment, including ground equipment, designed or modified for systems specified in 1.A., 19.A.1. or 19.A.2. Notes:
|
5D1 Software
The corresponding systems, equipment and components as identified in Council Regulation (EC) No 428/2009 of 5 May 2009 setting up a Community regime for the control of exports, transfer, brokering and transit of dual-use items |
Missile Technology Control Regime (M.TCR): Equipment, software and technology annex |
||
5D101 |
“Software” specially designed or modified for the “use” of equipment specified in 5A101. |
M12D3 |
“Software” specially designed or modified for the “use” of equipment specified in 12.A.4. or 12.A.5., usable for systems specified in 1.A., 19.A.1. or 19.A.2. |
5E1 Technology
The corresponding systems, equipment and components as identified in Council Regulation (EC) No 428/2009 of 5 May 2009 setting up a Community regime for the control of exports, transfer, brokering and transit of dual-use items |
Missile Technology Control Regime (M.TCR): Equipment, software and technology annex |
||
5E101 |
“Technology” according to the General Technology Note for the “development”, “production” or “use” of equipment specified in 5A101. |
M12E1 |
“Technology”, in accordance with the General Technology Note, for the “development”, “production” or “use” of equipment or “software” specified in 12.A. or 12.D. |
CATEGORY 6 — SENSORS AND LASERS
6A Systems, Equipment and Components
The corresponding systems, equipment and components as identified in Council Regulation (EC) No 428/2009 of 5 May 2009 setting up a Community regime for the control of exports, transfer, brokering and transit of dual-use items |
Missile Technology Control Regime (M.TCR): Equipment, software and technology annex |
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6A002 |
Optical sensors or equipment and components therefor, as follows:
|
M18A2 |
‘Detectors’ specially designed or modified to protect rocket systems and unmanned aerial vehicles against nuclear effects (e.g. Electromagnetic Pulse (EMP), X-rays, combined blast and thermal effects), and usable for the systems specified in 1.A. Technical Note: A ‘detector’ is defined as a mechanical, electrical, optical or chemical device that automatically identifies and records, or registers a stimulus such as an environmental change in pressure or temperature, an electrical or electromagnetic signal or radiation from a radioactive material. This includes devices that sense by one time operation or failure |
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M11A2 |
Passive sensors for determining bearings to specific electromagnetic sources (direction finding equipment) or terrain characteristics, designed or modified for use in the systems specified in 1.A. |
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6A006 |
“Magnetometers”, “magnetic gradiometers”, “intrinsic magnetic gradiometers”, underwater electric field sensors, “compensation systems”, and specially designed components therefor, as follows:
|
M9A8 |
Three axis magnetic heading sensors having all of the following characteristics, and specially designed components therefor:
|
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6A007 |
Gravity meters (gravimeters) and gravity gradiometers, as follows:
|
M12A3 |
Gravity meters (gravimeters) or gravity gradiometers, designed or modified for airborne or marine use, usable for systems specified in 1.A., as follows, and specially designed components therefor:
|
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6A008 |
Radar systems, equipment and assemblies, having any of the following, and specially designed components therefor:
|
M11A1 |
Radar and laser radar systems, including altimeters, designed or modified for use in the systems specified in 1.A. Technical Note: Laser radar systems embody specialised transmission, scanning, receiving and signal processing techniques for utilisation of lasers for echo ranging, direction finding and discrimination of targets by location, radial speed and body reflection characteristics. |
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M12A5b |
Range instrumentation radars including associated optical/infrared trackers with all of the following capabilities:
|
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6A102 |
Radiation hardened ‘detectors’, other than those specified in 6A002, specially designed modified for protecting against nuclear effects (e.g. electromagnetic pulse (EMP), X-rays, combined blast and thermal effects) and usable for “missiles”, designed or rated to withstand radiation levels which meet or exceed a total irradiation dose of 5 × 105 rads (silicon). Technical Note: In 6A102, a ‘detector’ is defined as a mechanical, electrical, optical or chemical device that automatically identifies and records, or registers a stimulus such as an environmental change in pressure or temperature, an electrical or electromagnetic signal or radiation from a radioactive material. This includes devices that sense by one time operation or failure. |
M18A2 |
‘Detectors’ specially designed or modified to protect rocket systems and unmanned aerial vehicles against nuclear effects (e.g. Electromagnetic Pulse (EMP), X-rays, combined blast and thermal effects), and usable for the systems specified in 1.A. Technical Note: A ‘detector’ is defined as a mechanical, electrical, optical or chemical device that automatically identifies and records, or registers a stimulus such as an environmental change in pressure or temperature, an electrical or electromagnetic signal or radiation from a radioactive material. This includes devices that sense by one time operation or failure. |
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6A107 |
Gravity meters (gravimeters) and components for gravity meters and gravity gradiometers, as follows:
|
M12A3 |
Gravity meters (gravimeters) or gravity gradiometers, designed or modified for airborne or marine use, usable for systems specified in 1.A., as follows, and specially designed components therefor:
|
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6A108 |
Radar systems and tracking systems, other than those specified in entry 6A008, as follows:
|
M11A1 |
Radar and laser radar systems, including altimeters, designed or modified for use in the systems specified in 1.A. Technical Note: Laser radar systems embody specialised transmission, scanning, receiving and signal processing techniques for utilisation of lasers for echo ranging, direction finding and discrimination of targets by location, radial speed and body reflection characteristics. |
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M12A5 |
Precision tracking systems, usable for systems specified in 1.A., 19.A.1. or 19.A.2. as follows:
|
6B Test, Inspection and Production Equipment
The corresponding systems, equipment and components as identified in Council Regulation (EC) No 428/2009 of 5 May 2009 setting up a Community regime for the control of exports, transfer, brokering and transit of dual-use items |
Missile Technology Control Regime (M.TCR): Equipment, software and technology annex |
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6B008 |
Pulse radar cross-section measurement systems having transmit pulse widths of 100 ns or less, and specially designed components therefor.
|
M17B1 |
Systems, specially designed for radar cross section measurement, usable for the systems specified in 1.A., 19.A.1. or 19.A.2. or the subsystems specified in 2.A |
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6B108 |
Systems, other than those specified in 6B008, specially designed for radar cross section measurement usable for ‘missiles’ and their subsystems. Technical Note: In 6B108 ‘missile’ means complete rocket systems and unmanned aerial vehicle systems capable of a range exceeding 300 km. |
M17B1 |
Systems, specially designed for radar cross section measurement, usable for the systems specified in 1.A., 19.A.1. or 19.A.2. or the subsystems specified in 2.A |
6D Software
The corresponding systems, equipment and components as identified in Council Regulation (EC) No 428/2009 of 5 May 2009 setting up a Community regime for the control of exports, transfer, brokering and transit of dual-use items |
Missile Technology Control Regime (M.TCR): Equipment, software and technology annex |
||
6D002 |
“Software” specially designed for the “use” of equipment specified in 6A002.b., 6A008 or 6B008. |
M |
Means specific information which is required for the “development”, “production” or “use” of a product. The information may take the form of “technical data” or “technical assistance”. |
6D102 |
“Software” specially designed or modified for the “use” of goods specified in 6A108. |
M11D1 |
“Software” specially designed or modified for the “use” of equipment specified in 11.A.1., 11.A.2. or 11.A.4. |
M12D3 |
“Software” specially designed or modified for the “use” of equipment specified in 12.A.4. or 12.A.5., usable for systems specified in 1.A., 19.A.1. or 19.A.2. |
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6D103 |
“Software” which processes post-flight, recorded data, enabling determination of vehicle position throughout its flight path, specially designed or modified for ‘missiles’. Technical Note: In 6D103 ‘missile’ means complete rocket systems and unmanned aerial vehicle systems capable of a range exceeding 300 km. |
M12D2 |
“Software” which processes post-flight, recorded data, enabling determination of vehicle position throughout its flight path, specially designed or modified for systems specified in 1.A., 19.A.1. or 19.A.2. |
6E Technology
The corresponding systems, equipment and components as identified in Council Regulation (EC) No 428/2009 of 5 May 2009 setting up a Community regime for the control of exports, transfer, brokering and transit of dual-use items |
Missile Technology Control Regime (M.TCR): Equipment, software and technology annex |
||||
6E001 |
“Technology” according to the General Technology Note for the “development” of equipment, materials or “software” specified in 6A, 6B, 6C or 6D. |
M |
Means specific information which is required for the “development”, “production” or “use” of a product. The information may take the form of “technical data” or “technical assistance”. |
||
6E002 |
“Technology” according to the General Technology Note for the “production” of equipment or materials specified in 6A, 6B or 6C. |
M |
Means specific information which is required for the “development”, “production” or “use” of a product. The information may take the form of “technical data” or “technical assistance”. |
||
6E101 |
“Technology” according to the General Technology Note for the “use” of equipment or “software” specified in 6A002, 6A007.b. and c., 6A008, 6A102, 6A107, 6A108, 6B108, 6D102 or 6D103.
|
M |
Means specific information which is required for the “development”, “production” or “use” of a product. The information may take the form of “technical data” or “technical assistance”. |
CATEGORY 7 — NAVIGATION AND AVIONICS
7A Systems, Equipment and Components
The corresponding systems, equipment and components as identified in Council Regulation (EC) No 428/2009 of 5 May 2009 setting up a Community regime for the control of exports, transfer, brokering and transit of dual-use items |
Missile Technology Control Regime (M.TCR): Equipment, software and technology annex |
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7A001 |
Accelerometers as follows and specially designed components therefor:
|
M9A3 |
Linear accelerometers, designed for use in inertial navigation systems or in guidance systems of all types, usable in the systems specified in 1.A., 19.A.1. or 19.A.2., having all of the following characteristics, and specially designed components therefor:
Technical Notes:
|
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M9A5 |
Accelerometers or gyros of any type, designed for use in inertial navigation systems or in guidance systems of all types, specified to function at acceleration levels greater than 100 g, and specially designed components therefor.
|
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7A002 |
Gyros or angular rate sensors, having any of the following and specially designed components therefor:
|
M9A4 |
All types of gyros usable in the systems specified in 1.A., 19.A.1 or 19.A.2., with a rated ‘drift rate’‘stability’ of less than 0,5 degrees (1 sigma or rms) per hour in a 1 g environment, and specially designed components therefor. Technical Notes:
|
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|
M9A5 |
Accelerometers or gyros of any type, designed for use in inertial navigation systems or in guidance systems of all types, specified to function at acceleration levels greater than 100 g, and specially designed components therefor.
|
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7A003 |
‘Inertial measurement equipment or systems’, having any of the following:
Technical Notes:
|
M2A1d |
‘Guidance sets’, usable in the systems specified in 1.A., capable of achieving system accuracy of 3,33 % or less of the “range” (e.g. a ‘CEP’ of 10 km or less at a “range” of 300 km), except as provided in the Note below 2.A.1. for those designed for missiles with a “range” under 300 km or manned aircraft; |
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M9A6 |
Inertial or other equipment using accelerometers specified in 9.A.3. or 9.A.5. or gyros specified in 9.A.4. or 9.A.5., and systems incorporating such equipment, and specially designed components therefor. |
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M9A8 |
Three axis magnetic heading sensors having all of the following characteristics, and specially designed components therefor:
|
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7A004 |
‘Star trackers’ and components therefor, as follows:
Technical Note: ‘Star trackers’ are also referred to as stellar attitude sensors or gyro-astro compasses. |
M9A2 |
Gyro-astro compasses and other devices which derive position or orientation by means of automatically tracking celestial bodies or satellites, and specially designed components therefor. |
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7A005 |
Global Navigation Satellite Systems (GNSS) receiving equipment having any of the following and specially designed components therefor:
|
M11A3 |
Receiving equipment for Global Navigation Satellite Systems (GNSS; e.g. GPS, GLONASS or Galileo), having any of the following characteristics, and specially designed components therefor:
|
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7A006 |
Airborne altimeters operating at frequencies other than 4,2 to 4,4 GHz inclusive and having any of the following:
|
M11A1 |
Radar and laser radar systems, including altimeters, designed or modified for use in the systems specified in 1.A. Technical Note: Laser radar systems embody specialised transmission, scanning, receiving and signal processing techniques for utilisation of lasers for echo ranging, direction finding and discrimination of targets by location, radial speed and body reflection characteristics. |
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7A101 |
Linear accelerometers, other than those specified in 7A001, designed for use in inertial navigation systems or in guidance systems of all types, usable in ‘missiles’, having all the following characteristics, and specially designed components therefor:
Technical Notes:
|
M9A3 |
Linear accelerometers, designed for use in inertial navigation systems or in guidance systems of all types, usable in the systems specified in 1.A., 19.A.1. or 19.A.2., having all of the following characteristics, and specially designed components therefor:
Technical Notes:
|
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7A102 |
All types of gyros, other than those specified in 7A002, usable in ‘missiles’, with a rated “drift rate”‘stability’ of less than 0,5° (1 sigma or rms) per hour in a 1 g environment and specially designed components therefor. Technical Notes:
|
M9A4 |
All types of gyros usable in the systems specified in 1.A., 19.A.1 or 19.A.2., with a rated ‘drift rate’‘stability’ of less than 0,5 degrees (1 sigma or rms) per hour in a 1 g environment, and specially designed components therefor. Technical Notes:
|
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7A103 |
Instrumentation, navigation equipment and systems, other than those specified in 7A003, as follows; and specially designed components therefor:
|
M9A6 |
Inertial or other equipment using accelerometers specified in 9.A.3. or 9.A.5. or gyros specified in 9.A.4. or 9.A.5., and systems incorporating such equipment, and specially designed components therefor. |
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M9A1 |
Integrated flight instrument systems which include gyrostabilisers or automatic pilots, designed or modified for use in the systems specified in 1.A., or 19.A.1. or 19.A.2. and specially designed components therefor. |
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M9A7 |
‘Integrated navigation systems’, designed or modified for the systems specified in 1.A., 19.A.1. or 19.A.2. and capable of providing a navigational accuracy of 200 m CEP or less. Technical Note: An ‘integrated navigation system’ typically incorporates all of the following components:
|
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Technical Note: In 7A103 ‘missile’ means complete rocket systems and unmanned aerial vehicle systems capable of a range exceeding 300 km. |
M9A8 |
Three axis magnetic heading sensors having all of the following characteristics, and specially designed components therefor:
|
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7A104 |
Gyro-astro compasses and other devices, other than those specified in 7A004, which derive position or orientation by means of automatically tracking celestial bodies or satellites and specially designed components therefor. |
M9A2 |
Gyro-astro compasses and other devices which derive position or orientation by means of automatically tracking celestial bodies or satellites, and specially designed components therefor. |
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7A105 |
Receiving equipment for Global Navigation Satellite Systems (GNSS; e.g. GPS, GLONASS, or Galileo), other than those specified in 7A005, having any of the following characteristics, and specially designed components therefor:
|
M11A3 |
Receiving equipment for Global Navigation Satellite Systems (GNSS; e.g. GPS, GLONASS or Galileo), having any of the following characteristics, and specially designed components therefor:
|
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7A106 |
Altimeters, other than those specified in 7A006, of radar or laser radar type, designed or modified for use in space launch vehicles specified in 9A004 or sounding rockets specified in 9A104. |
M11A1 |
Radar and laser radar systems, including altimeters, designed or modified for use in the systems specified in 1.A. Technical Note: Laser radar systems embody specialised transmission, scanning, receiving and signal processing techniques for utilisation of lasers for echo ranging, direction finding and discrimination of targets by location, radial speed and body reflection characteristics. |
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7A115 |
Passive sensors for determining bearing to specific electromagnetic source (direction finding equipment) or terrain characteristics, designed or modified for use in space launch vehicles specified in 9A004 or sounding rockets specified in 9A104.
|
M11A2 |
Passive sensors for determining bearings to specific electromagnetic sources (direction finding equipment) or terrain characteristics, designed or modified for use in the systems specified in 1.A. |
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7A116 |
Flight control systems and servo valves, as follows; designed or modified for use in space launch vehicles specified in 9A004 or sounding rockets specified in 9A104.
|
M10A1 |
Pneumatic, hydraulic, mechanical, electro-optical, or electromechanical flight control systems (including fly-by-wire and fly-by-light systems) designed or modified for the systems specified in 1.A. |
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M10A2 |
Attitude control equipment designed or modified for the systems specified in 1.A. |
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M10A3 |
Flight control servo valves designed or modified for the systems in 10.A.1. or 10.A.2., and designed or modified to operate in a vibration environment greater than 10 g rms between 20 Hz and 2 kHz.
|
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7A117 |
“Guidance sets”, usable in “missiles” capable of achieving system accuracy of 3,33 % or less of the range (e.g., a “CEP” of 10 km or less at a range of 300 km). |
M2A1d |
‘Guidance sets’, usable in the systems specified in 1.A., capable of achieving system accuracy of 3,33 % or less of the “range” (e.g. a ‘CEP’ of 10 km or less at a “range” of 300 km), except as provided in the Note below 2.A.1. for those designed for missiles with a “range” under 300 km or manned aircraft; |
7B Test, Inspection and Production Equipment
The corresponding systems, equipment and components as identified in Council Regulation (EC) No 428/2009 of 5 May 2009 setting up a Community regime for the control of exports, transfer, brokering and transit of dual-use items |
Missile Technology Control Regime (M.TCR): Equipment, software and technology annex |
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7B001 |
Test, calibration or alignment equipment, specially designed for equipment specified in 7A.
Technical Notes:
|
M2B2 |
“Production equipment” specially designed for the subsystems specified in 2.A. |
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M9B1 |
“Production equipment”, and other test, calibration and alignment equipment, other than that described in 9.B.2., designed or modified to be used with equipment specified in 9.A.
|
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M10B1 |
Test, calibration, and alignment equipment specially designed for equipment specified in 10.A. |
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7B002 |
Equipment specially designed to characterize mirrors for ring “laser” gyros, as follows:
|
M9B1 |
“Production equipment”, and other test, calibration and alignment equipment, other than that described in 9.B.2., designed or modified to be used with equipment specified in 9.A.
|
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7B003 |
Equipment specially designed for the “production” of equipment specified in 7A.
|
M2B2 |
“Production equipment” specially designed for the subsystems specified in 2.A. |
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M9B1 |
“Production equipment”, and other test, calibration and alignment equipment, other than that described in 9.B.2., designed or modified to be used with equipment specified in 9.A.
|
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7B102 |
Reflectometers specially designed to characterise mirrors, for “laser” gyros, having a measurement accuracy of 50 ppm or less (better). |
M9B1 |
“Production equipment”, and other test, calibration and alignment equipment, other than that described in 9.B.2., designed or modified to be used with equipment specified in 9.A.
|
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7B103 |
“Production facilities” and “production equipment” as follows: |
|
|
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|
M2B1 |
“Production facilities” specially designed for the subsystems specified in 2.A |
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M2B2* |
“Production equipment” specially designed for the subsystems specified in 2.A. |
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M9B1 |
“Production equipment”, and other test, calibration and alignment equipment, other than that described in 9.B.2., designed or modified to be used with equipment specified in 9.A.
|
7D Software
The corresponding systems, equipment and components as identified in Council Regulation (EC) No 428/2009 of 5 May 2009 setting up a Community regime for the control of exports, transfer, brokering and transit of dual-use items |
Missile Technology Control Regime (M.TCR): Equipment, software and technology annex |
|||||||
7D002 |
“Source code” for the operation or maintenance of any inertial navigation equipment, including inertial equipment not specified in 7A003 or 7A004, or Attitude and Heading Reference Systems (‘AHRS’).
Technical Note: ‘AHRS’ generally differ from Inertial Navigation Systems (INS) in that an ‘AHRS’ provides attitude and heading information and normally does not provide the acceleration, velocity and position information associated with an INS. |
M2D3 |
“Software”, specially designed or modified for the operation or maintenance of ‘guidance sets’ specified in 2.A.1.d.
|
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M9D1 |
“Software” specially designed or modified for the “use” of equipment specified in 9.A. or 9.B. |
|||||||
7D101 |
“Software” specially designed or modified for the “use” of equipment specified in 7A001 to 7A006, 7A101 to 7A106, 7A115, 7A116.a., 7A116.b., 7B001, 7B002, 7B003, 7B102 or 7B103. |
M2D |
“Software” specially designed or modified for the “use” of “production facilities” specified in 2.B.1. |
|||||
M9D1 |
“Software” specially designed or modified for the “use” of equipment specified in 9.A. or 9.B. |
|||||||
M10D1 |
“Software” specially designed or modified for the “use” of equipment specified in 10.A. or 10.B.
|
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M11D1&2 |
“Software” specially designed or modified for the “use” of equipment specified in 11.A.1., 11.A.2. or 11.A.4. “Software” specially designed for the “use” of equipment specified in 11.A.3. |
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7D102 |
Integration “software” as follows:
|
M9D2 |
Integration “software” for the equipment specified in 9.A.1. |
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|
M9D3* |
Integration “software” specially designed for the equipment specified in 9.A.6. |
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|
M9D4 |
Integration “software”, designed or modified for the ‘integrated navigation systems’ specified in 9.A.7.
|
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7D103 |
“Software” specially designed for modelling or simulation of the “guidance sets” specified in 7A117 or for their design integration with the space launch vehicles specified in 9A004 or sounding rockets specified in 9A104.
|
M16D1 |
“Software” specially designed for modelling, simulation, or design integration of the systems specified in 1.A. or the subsystems specified in 2.A or 20.A.
|
7E Technology
The corresponding systems, equipment and components as identified in Council Regulation (EC) No 428/2009 of 5 May 2009 setting up a Community regime for the control of exports, transfer, brokering and transit of dual-use items |
Missile Technology Control Regime (M.TCR): Equipment, software and technology annex |
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7E001 |
“Technology” according to the General Technology Note for the “development” of equipment or “software”, specified in 7A, 7B, 7D001, 7D002, 7D003, 7D005 and 7D101 to 7D103.
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M |
Means specific information which is required for the “development”, “production” or “use” of a product. The information may take the form of “technical data” or “technical assistance”. |
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7E002 |
“Technology” according to the General Technology Note for the “production” of equipment specified in 7A or 7B. |
M |
Means specific information which is required for the “development”, “production” or “use” of a product. The information may take the form of “technical data” or “technical assistance”. |
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7E003 |
“Technology” according to the General Technology Note for the repair, refurbishing or overhaul of equipment specified in 7A001 to 7A004.
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M2E1 |
“Technology”, in accordance with the General Technology Note, for the “development”, “production” or “use” of equipment or “software” specified in 2.A., 2.B. or 2.D. |
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M9E1 |
“Technology”, in accordance with the General Technology Note, for the “development”, “production” or “use” of equipment or “software” specified in 9.A., 9.B. or 9.D.
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7E004 |
Other “technology” as follows:
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M10E1 |
Design “technology” for integration of air vehicle fuselage, propulsion system and lifting control surfaces, designed or modified for the systems specified in 1.A. or 19.A.2., to optimise aerodynamic performance throughout the flight regime of an unmanned aerial vehicle. |
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7E101 |
“Technology” according to the General Technology Note for the “use” of equipment specified in 7A001 to 7A006, 7A101 to 7A106, 7A115 to 7A117, 7B001, 7B002, 7B003, 7B102, 7B103, 7D101 to 7D103. |
M |
Means specific information which is required for the “development”, “production” or “use” of a product. The information may take the form of “technical data” or “technical assistance”. |
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7E102 |
“Technology” for protection of avionics and electrical subsystems against electromagnetic pulse (EMP) and electromagnetic interference (EMI) hazards, from external sources, as follows:
|
M11E1 |
Design “technology” for protection of avionics and electrical subsystems against Electromagnetic Pulse (EMP) and Electromagnetic Interference (EMI) hazards from external sources, as follows:
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7E104 |
“Technology” for the integration of the flight control, guidance, and propulsion data into a flight management system for optimization of rocket system trajectory. |
M10E2 |
Design “technology” for integration of the flight control, guidance, and propulsion data into a flight management system, designed or modified for the systems specified in 1.A. or 19.A.1., for optimisation of rocket system trajectory. |
CATEGORY 9 — AEROSPACE AND PROPULSION
9A Systems, Equipment and Components
The corresponding systems, equipment and components as identified in Council Regulation (EC) No 428/2009 of 5 May 2009 setting up a Community regime for the control of exports, transfer, brokering and transit of dual-use items |
Missile Technology Control Regime (M.TCR): Equipment, software and technology annex |
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9A001 |
Aero gas turbine engines having any of the following:
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M3A1 |
Turbojet and turbofan engines, as follows:
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9A004 |
Space launch vehicles, “spacecraft”, “spacecraft buses”, “spacecraft payloads”, “spacecraft” on-board systems or equipment, and terrestrial equipment, as follows:
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M1A1 |
Complete rocket systems (including ballistic missile systems, space launch vehicles, and sounding rockets) capable of delivering at least a 500 kg “payload” to a “range” of at least 300 km. |
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M19A1 |
Complete rocket systems (including ballistic missile systems, space launch vehicles, and sounding rockets), not specified in 1.A.1., capable of a “range” equal to or greater than 300 km. |
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9A005 |
Liquid rocket propulsion systems containing any of the systems or components, specified in 9A006.
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M2A1a |
Individual rocket stages usable in the systems specified in 1.A.; |
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M2A1c |
Rocket propulsion subsystems, usable in the systems specified in 1.A., as follows;
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M20A1 |
Complete subsystems as follows:
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9A006 |
Systems and components, specially designed for liquid rocket propulsion systems, as follows:
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M3A8 |
Liquid propellant tanks specially designed for the propellants controlled in Item 4.C. or other liquid propellants used in the systems specified in 1.A.1. |
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M3A5 |
Liquid, slurry and gel propellant (including oxidisers) control systems, and specially designed components therefor, usable in the systems specified in 1.A., designed or modified to operate in vibration environments greater than 10 g rms between 20 Hz and 2 kHz. Notes:
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M3A10 |
Combustion chambers and nozzles for liquid propellant rocket engines usable in the subsystems specified in 2.A.1.c.2. or 20.A.1.b.2. |
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M3A8 |
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M3A5 |
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M3A10 |
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9A007 |
Solid rocket propulsion systems having any of the following:
|
M2A1 |
Complete subsystems usable in the systems specified in 1.A., as follows:
Solid propellant rocket motors or hybrid rocket motors having a total impulse capacity equal to or greater than 1,1 × 106 Ns; |
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M2A1c1 |
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9A008 |
Components specially designed for solid rocket propulsion systems, as follows:
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M3A3 |
Rocket motor cases, ‘insulation’ components and nozzles therefor, usable in the systems specified in 1.A. or 19.A.1. Technical Note: In 3.A.3. ‘insulation’ intended to be applied to the components of a rocket motor, i.e. the case, nozzle inlets, case closures, includes cured or semi-cured compounded rubber components comprising sheet stock containing an insulating or refractory material. It may also be incorporated as stress relief boots or flaps.
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M3C1 |
‘Interior lining’ usable for rocket motor cases in the subsystems specified in 2.A.1.c.1. or specially designed for subsystems specified in 20.A.1.b.1. Technical Note: In 3.C.1. ‘interior lining’ suited for the bond interface between the solid propellant and the case or insulating liner is usually a liquid polymer based dispersion of refractory or insulating materials e.g. carbon filled HTPB or other polymer with added curing agents to be sprayed or screeded over a case interior. |
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M3C2 |
‘Insulation’ material in bulk form usable for rocket motor cases in the subsystems specified in 2.A.1.c.1. or specially designed for subsystems specified in 20.A.1.b.1. Technical Note: In 3.C.2. ‘insulation’ intended to be applied to the components of a rocket motor, i.e. the case, nozzle inlets, case closures, includes cured or semi-cured compounded rubber sheet stock containing an insulating or refractory material. It may also be incorporated as stress relief boots or flaps specified in 3.A.3. |
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M2A1e |
Thrust vector control subsystems, usable in the systems specified in 1.A., except as provided in the Note below 2.A.1. for those designed for rocket systems that do not exceed the “range”/“payload” capability of systems specified in 1.A.; Technical Note: 2.A.1.e. includes the following methods of achieving thrust vector control:
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9A009 |
Hybrid rocket propulsion systems having any of the following:
|
M2A1c1 |
Solid propellant rocket motors or hybrid rocket motors having a total impulse capacity equal to or greater than 1,1 × 106 Ns; |
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M20A1b |
Rocket propulsion subsystems, not specified in 2.A.1., usable in the systems specified in 19.A.1., as follows:
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9A010 |
Specially designed components, systems and structures, for launch vehicles, launch vehicle propulsion systems or “spacecraft”, as follows:
|
M6A1 |
Composite structures, laminates, and manufactures thereof, specially designed for use in the systems specified in 1.A., 19.A.1. or 19.A.2. and the subsystems specified in 2.A. or 20.A. |
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M6A1 |
Composite structures, laminates, and manufactures thereof, specially designed for use in the systems specified in 1.A., 19.A.1. or 19.A.2. and the subsystems specified in 2.A. or 20.A. |
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M6A1 |
Composite structures, laminates, and manufactures thereof, specially designed for use in the systems specified in 1.A., 19.A.1. or 19.A.2. and the subsystems specified in 2.A. or 20.A. |
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M3A2 |
Ramjet/scramjet/pulse jet/‘combined cycle engines’, including devices to regulate combustion, and specially designed components therefor, usable in the systems specified in 1.A. or 19.A.2. Technical Note: In Item 3.A.2., ‘combined cycle engines’ are the engines that employ two or more cycles of the following types of engines: gas-turbine engine (turbojet, turboprop, turbofan and turboshaft), ramjet, scramjet, pulse jet, pulse detonation engine, rocket motor (liquid/solid-propellant and hybrid). |
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9A011 |
Ramjet, scramjet or combined cycle engines, and specially designed components therefor.
|
M3A2 |
Ramjet/scramjet/pulse jet/‘combined cycle engines’, including devices to regulate combustion, and specially designed components therefor, usable in the systems specified in 1.A. or 19.A.2. Technical Note: In Item 3.A.2., ‘combined cycle engines’ are the engines that employ two or more cycles of the following types of engines: gas-turbine engine (turbojet, turboprop, turbofan and turboshaft), ramjet, scramjet, pulse jet, pulse detonation engine, rocket motor (liquid/solid-propellant and hybrid). |
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9A012 |
“Unmanned aerial vehicles” (“UAVs”), unmanned “airships”, related equipment and components, as follows:
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M1A2 |
Complete unmanned aerial vehicle systems (including cruise missile systems, target drones and reconnaissance drones) capable of delivering at least a 500 kg “payload” to a “range” of at least 300 km. |
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M19A |
ITEM 19 OTHER COMPLETE DELIVERY SYSTEMS: equipment, assemblies and components |
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M9A6 |
Inertial or other equipment using accelerometers specified in 9.A.3. or 9.A.5. or gyros specified in 9.A.4. or 9.A.5., and systems incorporating such equipment, and specially designed components therefor. |
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9A101 |
Turbojet and turbofan engines, other than those specified in 9A001, as follows;
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M3A1 |
Turbojet and turbofan engines, as follows:
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9A102 |
‘Turboprop engine systems’ specially designed for unmanned aerial vehicles specified in 9A012 or 9A112.a., and specially designed components therefor, having a ‘maximum power’ greater than 10 kW.
Technical Notes:
|
M3A9 |
‘Turboprop engine systems’ specially designed for the systems in 1.A.2. or 19.A.2., and specially designed components therefor, having a maximum power greater than 10 kW (achieved uninstalled at sea level static conditions using the ICAO standard atmosphere), excluding civil certified engines. Technical Note: For the purposes of Item 3.A.9., a ‘turboprop engine system’ incorporates all of the following: a. Turboshaft engine; and b. Power transmission system to transfer the power to a propeller. |
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9A104 |
Sounding rockets, capable of a range of at least 300 km.
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M1A1 |
Complete rocket systems (including ballistic missile systems, space launch vehicles, and sounding rockets) capable of delivering at least a 500 kg “payload” to a “range” of at least 300 km. |
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M19A1 |
Complete rocket systems (including ballistic missile systems, space launch vehicles, and sounding rockets), not specified in 1.A.1., capable of a “range” equal to or greater than 300 km. |
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9A105 |
Liquid propellant rocket engines, as follows:
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M2A1c2 |
Liquid propellant rocket engines or gel propellant rocket motors integrated, or designed or modified to be integrated, into a liquid propellant or gel propellant propulsion system which has a total impulse capacity equal to or greater than 1,1 × 106 Ns; |
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M20A1b2 |
Liquid propellant rocket engines or gel propellant rocket motors integrated, or designed or modified to be integrated, into a liquid propellant or gel propellant propulsion system which has a total impulse capacity equal to or greater than 8,41 × 105 Ns, but less than 1,1 × 106 Ns |
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9A106 |
Systems or components, other than those specified in 9A006 as follows, specially designed for liquid rocket propulsion systems:
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M3A3 |
Rocket motor cases, ‘insulation’ components and nozzles therefor, usable in the systems specified in 1.A. or 19.A.1. Technical Note: In 3.A.3. ‘insulation’ intended to be applied to the components of a rocket motor, i.e. the case, nozzle inlets, case closures, includes cured or semi-cured compounded rubber components comprising sheet stock containing an insulating or refractory material. It may also be incorporated as stress relief boots or flaps.
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M2A1e |
Thrust vector control subsystems, usable in the systems specified in 1.A., except as provided in the Note below 2.A.1. for those designed for rocket systems that do not exceed the “range”/“payload” capability of systems specified in 1.A.; Technical Technical Note: 2.A.1.e. includes the following methods of achieving thrust vector control:
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M3A5 |
Liquid, slurry and gel propellant (including oxidisers) control systems, and specially designed components therefor, usable in the systems specified in 1.A., designed or modified to operate in vibration environments greater than 10 g rms between 20 Hz and 2 kHz. Notes:
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M3A10 |
Combustion chambers and nozzles for liquid propellant rocket engines usable in the subsystems specified in 2.A.1.c.2. or 20.A.1.b.2. |
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9A107 |
Solid propellant rocket engines, usable in complete rocket systems or unmanned aerial vehicles, capable of a range of 300 km, other than those specified in 9A007, having total impulse capacity equal to or greater than 0,841 MNs.
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M20A1b1 |
Solid propellant rocket motors or hybrid rocket motors having a total impulse capacity equal to or greater than 8,41 × 105 Ns, but less than 1,1 × 106 Ns; |
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9A108 |
Components, other than those specified in 9A008, as follows, specially designed for solid rocket propulsion systems:
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M3A3 |
Rocket motor cases, ‘insulation’ components and nozzles therefor, usable in the systems specified in 1.A. or 19.A.1. |
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M3A3 |
Technical Note: In 3.A.3. ‘insulation’ intended to be applied to the components of a rocket motor, i.e. the case, nozzle inlets, case closures, includes cured or semi-cured compounded rubber components comprising sheet stock containing an insulating or refractory material. It may also be incorporated as stress relief boots or flaps.
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M2A1e |
Thrust vector control subsystems, usable in the systems specified in 1.A., except as provided in the Note below 2.A.1. for those designed for rocket systems that do not exceed the “range”/“payload” capability of systems specified in 1.A.; Technical Note: 2.A.1.e. includes the following methods of achieving thrust vector control:
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9A109 |
Hybrid rocket motors and specially designed components as follows:
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M3A6 |
Specially designed components for hybrid rocket motors specified in 2.A.1.c.1. and 20.A.1.b.1. |
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M20A1b |
Rocket propulsion subsystems, not specified in 2.A.1., usable in the systems specified in 19.A.1., as follows:
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M2A1c |
Rocket propulsion subsystems, usable in the systems specified in 1.A., as follows;
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9A110 |
Composite structures, laminates and manufactures thereof, other than those specified in 9A010, specially designed for use in ‘missiles’ or the subsystems specified in 9A005, 9A007, 9A105, 9A106.c., 9A107, 9A108.c., 9A116 or 9A119.
Technical Note: In 9A110 ‘missile’ means complete rocket systems and unmanned aerial vehicle systems capable of a range exceeding 300 km. |
M6A1 |
Composite structures, laminates, and manufactures thereof, specially designed for use in the systems specified in 1.A., 19.A.1. or 19.A.2. and the subsystems specified in 2.A. or 20.A. |
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9A111 |
Pulse jet engines, usable in “missiles” or unmanned aerial vehicles specified in 9A012 or 9A112.a., and specially designed components therefor.
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M3A2 |
Ramjet/scramjet/pulse jet/‘combined cycle engines’, including devices to regulate combustion, and specially designed components therefor, usable in the systems specified in 1.A. or 19.A.2. Technical Note: In Item 3.A.2., ‘combined cycle engines’ are the engines that employ two or more cycles of the following types of engines: gas-turbine engine (turbojet, turboprop, turbofan and turboshaft), ramjet, scramjet, pulse jet, pulse detonation engine, rocket motor (liquid/solid-propellant and hybrid) |
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9A112 |
“Unmanned aerial vehicles” (“UAVs”), other than those specified in 9A012, as follows:
|
M19A2 |
Complete unmanned aerial vehicle systems (including cruise missile systems, target drones and reconnaissance drones), not specified in 1.A.2., capable of a “range” equal to or greater than 300 km. |
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M19A3 |
Complete unmanned aerial vehicle systems, not specified in 1.A.2. or 19.A.2., having all of the following:
Technical Notes:
|
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9A115 |
Launch support equipment as follows:
|
M12A1 |
Apparatus and devices, designed or modified for the handling, control, activation and launching of the systems specified in 1.A., 19.A.1., or 19.A.2. |
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M12A2 |
Vehicles designed or modified for the transport, handling, control, activation and launching of the systems specified in 1.A. |
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9A116 |
Reentry vehicles, usable in “missiles”, and equipment designed or modified therefor, as follows:
|
M2A1b |
Re-entry vehicles, and equipment designed or modified therefor, usable in the systems specified in 1.A., as follows, except as provided in the Note below 2.A.1. for those designed for non-weapon payloads:
|
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9A117 |
Staging mechanisms, separation mechanisms, and interstages, usable in “missiles”.
|
M3A4 |
Staging mechanisms, separation mechanisms, and interstages therefor, usable in the systems specified in 1.A.
Technical Note: Staging and separation mechanisms specified in 3.A.4. may contain some of the following components:
|
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9A118 |
Devices to regulate combustion usable in engines, which are usable in “missiles” or unmanned aerial vehicles specified in 9A012 or 9A112.a., specified in 9A011 or 9A111. |
M3A2 |
Ramjet/scramjet/pulse jet/‘combined cycle engines’, including devices to regulate combustion, and specially designed components therefor, usable in the systems specified in 1.A. or 19.A.2. Technical Note: In Item 3.A.2., ‘combined cycle engines’ are the engines that employ two or more cycles of the following types of engines: gas-turbine engine (turbojet, turboprop, turbofan and turboshaft), ramjet, scramjet, pulse jet, pulse detonation engine, rocket motor (liquid/solid-propellant and hybrid). |
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9A119 |
Individual rocket stages, usable in complete rocket systems or unmanned aerial vehicles, capable of a range of 300 km, other than those specified in 9A005, 9A007, 9A009, 9A105, 9A107 and 9A109. |
M2A1a |
Individual rocket stages usable in the systems specified in 1.A.; |
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M20A1a |
Complete subsystems as follows: a. Individual rocket stages, not specified in 2.A.1., usable in systems specified in 19.A. |
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9A120 |
Liquid propellant tanks, other than those specified in 9A006, specially designed for propellants specified in 1C111 or ‘other liquid propellants’, used in rocket systems capable of delivering at least a 500 kg payload to a range of at least 300 km. |
M3A8 |
Liquid propellant tanks specially designed for the propellants controlled in Item 4.C. or other liquid propellants used in the systems specified in 1.A.1. |
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9A121 |
Umbilical and interstage electrical connectors specially designed for “missiles”, space launch vehicles specified in 9A004 or sounding rockets specified in 9A104. Technical Note: Interstage connectors referred to in 9A121 also include electrical connectors installed between the “missile”, space launch vehicle or sounding rocket and their payload. |
M11A5 |
Umbilical and interstage electrical connectors specially designed for systems specified in 1.A.1. or 19.A.1. Technical Note: Interstage connectors referred to in 11.A.5. also include electrical connectors installed between systems specified in 1.A.1. or 19.A.1. and their “payload”. |
9B Test, Inspection and Production Equipment
The corresponding systems, equipment and components as identified in Council Regulation (EC) No 428/2009 of 5 May 2009 setting up a Community regime for the control of exports, transfer, brokering and transit of dual-use items |
Missile Technology Control Regime (M.TCR): Equipment, software and technology annex |
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9B005 |
On-line (real time) control systems, instrumentation (including sensors) or automated data acquisition and processing equipment, specially designed for use with any of the following:
|
M15B2 |
‘Aerodynamic test facilities’ for speeds of Mach 0,9 or more, usable for the systems specified in 1.A. or 19.A. or the subsystems specified in 2.A. or 20.A.
Technical Notes:
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9B006 |
Acoustic vibration test equipment capable of producing sound pressure levels of 160 dB or more (referenced to 20 μPa) with a rated output of 4 kW or more at a test cell temperature exceeding 1 273 K (1 000 °C), and specially designed quartz heaters therefor.
|
M15B4b |
Environmental chambers capable of simulating all of the following flight conditions:
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9B105 |
‘Aerodynamic test facilities’ for speeds of Mach 0,9 or more, usable for ‘missiles’ and their subsystems.
Technical Notes:
|
M15B2 |
‘Aerodynamic test facilities’ for speeds of Mach 0,9 or more, usable for the systems specified in 1.A. or 19.A. or the subsystems specified in 2.A. or 20.A.
Technical Notes:
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9B106 |
Environmental chambers and anechoic chambers, as follows:
|
M15B4 |
Environmental chambers as follows, usable for the systems specified in 1.A. or 19.A. or the subsystems specified in 2.A. or 20.A.:
|
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9B115 |
Specially designed “production equipment” for the systems, sub-systems and components specified in 9A005 to 9A009, 9A011, 9A101, 9A102, 9A105 to 9A109, 9A111, 9A116 to 9A120. |
M2B2 |
“Production equipment” specially designed for the subsystems specified in 2.A. |
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M3B2 |
“Production equipment” specially designed for equipment or materials specified in 3.A.1., 3.A.2., 3.A.3., 3.A.4., 3.A.5., 3.A.6., 3.A.8., 3.A.9., 3.A.10. or 3.C. |
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M20B2 |
“Production equipment” specially designed for the subsystems specified in 20.A. |
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9B116 |
Specially designed “production facilities” for the space launch vehicles specified in 9A004, or systems, sub-systems, and components specified in 9A005 to 9A009, 9A011, 9A101, 9A102, 9A104 to 9A109, 9A111, 9A116 to 9A120 or ‘missiles’. Technical Note: In 9B116 ‘missile’ means complete rocket systems and unmanned aerial vehicle systems capable of a range exceeding 300 km. |
M1B1 |
“Production facilities” specially designed for the systems specified in 1.A |
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M2B1 |
“Production facilities” specially designed for the subsystems specified in 2.A. |
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M3B1 |
“Production facilities” specially designed for equipment or materials specified in 3.A.1., 3.A.2., 3.A.3., 3.A.4., 3.A.5., 3.A.6., 3.A.8., 3.A.9., 3.A.10. or 3.C. |
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M19B1 |
“Production facilities” specially designed for the systems specified in 19.A.1 or 19.A.2. |
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M20B1 |
“Production facilities” specially designed for the subsystems specified in 20.A. |
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9B117 |
Test benches and test stands for solid or liquid propellant rockets or rocket motors, having either of the following characteristics:
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M15B3 |
Test benches/stands, usable for the systems specified in 1.A., 19.A.1. or 19.A.2. or the subsystems specified in 2.A. or 20.A., which have the capacity to handle solid or liquid propellant rockets, motors or engines having a thrust greater than 68 kN, or which are capable of simultaneously measuring the three axial thrust components. |
9C Materials
The corresponding systems, equipment and components as identified in Council Regulation (EC) No 428/2009 of 5 May 2009 setting up a Community regime for the control of exports, transfer, brokering and transit of dual-use items |
Missile Technology Control Regime (M.TCR): Equipment, software and technology annex |
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9C108 |
“Insulation” material in bulk form and “interior lining”, other than those specified in 9A008, for rocket motor cases usable in “missiles” or specially designed for ‘missiles’. Technical Note: In 9C108 ‘missile’ means complete rocket systems and unmanned aerial vehicle systems capable of a range exceeding 300 km. |
M3C1 |
‘Interior lining’ usable for rocket motor cases in the subsystems specified in 2.A.1.c.1. or specially designed for subsystems specified in 20.A.1.b.1. Technical Note: In 3.C.1. ‘interior lining’ suited for the bond interface between the solid propellant and the case or insulating liner is usually a liquid polymer based dispersion of refractory or insulating materials e.g. carbon filled HTPB or other polymer with added curing agents to be sprayed or screeded over a case interior. |
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M3C2 |
‘Insulation’ material in bulk form usable for rocket motor cases in the subsystems specified in 2.A.1.c.1. or specially designed for subsystems specified in 20.A.1.b.1. Technical Note: In 3.C.2. ‘insulation’ intended to be applied to the components of a rocket motor, i.e. the case, nozzle inlets, case closures, includes cured or semi-cured compounded rubber sheet stock containing an insulating or refractory material. It may also be incorporated as stress relief boots or flaps specified in 3.A.3. |
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9C110 |
Resin impregnated fibre prepregs and metal coated fibre preforms therefor, for composite structures, laminates and manufactures specified in 9A110, made either with organic matrix or metal matrix utilising fibrous or filamentary reinforcements having a “specific tensile strength” greater than 7,62 × 104 m and a “specific modulus” greater than 3,18 × 106 m.
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M6C1 |
Resin impregnated fibre prepregs and metal coated fibre preforms, for the goods specified in 6.A.1., made either with organic matrix or metal matrix utilising fibrous or filamentary reinforcements having a specific tensile strength greater than 7,62 × 104 m and a specific modulus greater than 3,18 × 106 m.
Technical Notes:
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9D Software
The corresponding systems, equipment and components as identified in Council Regulation (EC) No 428/2009 of 5 May 2009 setting up a Community regime for the control of exports, transfer, brokering and transit of dual-use items |
Missile Technology Control Regime (M.TCR): Equipment, software and technology annex |
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9D001 |
“Software” specially designed or modified for the “development” of equipment or “technology”, specified in 9A001 to 9A119, 9B or 9E003. |
M3D3 |
“Software” specially designed or modified for the “development” of equipment specified in 3.A.2., 3.A.3. or 3.A.4. |
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9D002 |
“Software” specially designed or modified for the “production” of equipment specified in 9A001 to 9A119 or 9B. |
M2D2 |
“Software” specially designed or modified for the “use” of rocket motors or engines specified in 2.A.1.c. |
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9D004 |
Other “software” as follows:
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M19D1 |
“Software” which coordinates the function of more than one subsystem, specially designed or modified for “use” in the systems specified in 19.A.1. or 19.A.2. |
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9D101 |
“Software” specially designed or modified for the “use” of goods specified in 9B105, 9B106, 9B116 or 9B117. |
M1D1 |
“Software” specially designed or modified for the “use” of “production facilities” specified in 1.B. |
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M2D1 |
“Software” specially designed or modified for the “use” of “production facilities” specified in 2.B.1. |
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M3D1 |
“Software” specially designed or modified for the “use” of “production facilities” and flow-forming machines specified in 3.B.1. or 3.B.3. |
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M12D1 |
“Software” specially designed or modified for the “use” of equipment specified in 12.A.1. |
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M15D1 |
“Software” specially designed or modified for the “use” of equipment specified in 15.B. usable for testing systems specified in 1.A., 19.A.1. or 19.A.2. or subsystems specified in 2.A. or 20.A. |
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M20D1 |
“Software” specially designed or modified for the systems specified in 20.B.1. |
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9D103 |
“Software” specially designed for modelling, simulation or design integration of the space launch vehicles specified in 9A004, sounding rockets specified in 9A104 or “missiles”, or the subsystemsspecified in 9A005, 9A007, 9A105, 9A106.c., 9A107, 9A108.c., 9A116 or 9A119.
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M16D1 |
“Software” specially designed for modelling, simulation, or design integration of the systems specified in 1.A. or the subsystems specified in 2.A or 20.A. Technical Note: The modelling includes in particular the aerodynamic and thermodynamic analysis of the systems. |
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9D104 |
“Software” specially designed or modified for the “use” of goods specified in 9A001, 9A005, 9A006.d., 9A006.g., 9A007.a., 9A008.d., 9A009.a., 9A010.d., 9A011, 9A101, 9A102, 9A105, 9A106.c., 9A106.d., 9A107, 9A108.c., 9A109, 9A111, 9A115.a., 9A116.d., 9A117 or 9A118. |
M2D2 M2D4 M3D2 M2D5 M20D2 |
“Software” specially designed or modified for the “use” of rocket motors or engines specified in 2.A.1.c. “Software” specially designed or modified for the operation or maintenance of subsystems or equipment specified in 2.A.1.b.3. “Software” specially designed or modified for the “use” of equipment specified in 3.A.1., 3.A.2., 3.A.4., 3.A.5., 3.A.6. or 3.A.9. Notes:
“Software” specially designed or modified for the operation or maintenance of subsystems in 2.A.1.e. “Software”, not specified in 2.D.2., specially designed or modified for the “use” of rocket motors or engines specified in 20.A.1.b. |
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9D105 |
“Software” which coordinates the function of more than one subsystem, other than that specified in 9D003.e., specially designed or modified for “use” in space launch vehicles specified in 9A004 or sounding rockets specified in 9A104 or ‘missiles’. Technical Note: In 9D105 ‘missile’ means complete rocket systems and unmanned aerial vehicle systems capable of a range exceeding 300 km. |
M1D2 |
“Software” specially designed or modified to coordinate the function of more than one subsystem in systems specified in 1.A. |
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M19D1 |
“Software” which coordinates the function of more than one subsystem, specially designed or modified for “use” in the systems specified in 19.A.1. or 19.A.2. |
9E Technology
The corresponding systems, equipment and components as identified in Council Regulation (EC) No 428/2009 of 5 May 2009 setting up a Community regime for the control of exports, transfer, brokering and transit of dual-use items |
Missile Technology Control Regime (M.TCR): Equipment, software and technology annex |
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9E001 |
“Technology” according to the General Technology Note for the “development” of equipment |
M |
Means specific information which is required for the “development”, “production” or “use” of a product. The information may take the form of “technical data” or “technical assistance”. |
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9E002 |
“Technology” according to the General Technology Note for the “production” of equipment materials, see 1E002.f. |
M |
Means specific information which is required for the “development”, “production” or “use” of a product. The information may take the form of “technical data” or “technical assistance”. |
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9E101 |
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M |
Means specific information which is required for the “development”, “production” or “use” of a product. The information may take the form of “technical data” or “technical assistance”. |
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9E102 |
“Technology” according to the General Technology Note for the “use” of space launch vehicles specified in9A004, goods specified in 9A005 to 9A011, ‘UAV’s specified in 9A012 or goods specified in 9A101, 9A102, 9A104 to 9A111, 9A112.a., 9A115 to 9A121, 9B105, 9B106, 9B115, 9B116, 9B117, 9D101 or 9D103. Technical Note: In 9E102 ‘UAV’ means unmanned aerial vehicle systems capable of a range exceeding 300 km. |
M |
Means specific information which is required for the “development”, “production” or “use” of a product. The information may take the form of “technical data” or “technical assistance”.’ |
ANNEX III
‘ANNEX VIIB
Graphite and raw, fabricated semi-finished metals referred to in Article 15a
HS Codes and descriptions
1. |
Raw or semi-fabricated graphite
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2. |
Corrosion-resistant high-grade steel (Chromium-content > 12 %) in form of sheet, plate, tube or bar
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3. |
Aluminium and alloys in form of sheet, plate, tube or bar
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4. |
Titanium and alloys in form of sheet, plate, tube or bar
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5. |
Nickel and alloys in form of sheet, plate, tube or bar
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Explanatory note: the metal alloys in points 2, 3, 4 and 5 are those containing a higher percentage by weight of the stated metal than of any other element.’