6.1.2022
1C011
EN
Official Journal of the European Union
L 3/57
a. (continued) Technical Note: The natural content of hafnium in the zirconium (typically 2 % to 7 %) is counted with the zirconium.
Note: The metals or alloys specified in 1C011.a. are controlled whether or not the metals or alloys are encapsulated in aluminium, magnesium, zirconium or beryllium. b.
Boron or boron alloys, with a particle size of 60 μm or less, as follows: 1.
Boron with a purity of 85 % by weight or more; 2.
Boron alloys with a boron content of 85 % by weight or more; Note: The metals or alloys specified in 1C011.b. are controlled whether or not the metals or alloys are encapsulated in aluminium, magnesium, zirconium or beryllium. c.
Guanidine nitrate (CAS 506-93-4); d.
Nitroguanidine (NQ) (CAS 556-88-7).
N.B. See also Military Goods Controls for metal powders mixed with other substances to form a mixture formulated for military purposes.
1C012
Materials as follows: Technical Note: These materials are typically used for nuclear heat sources. a.
Plutonium in any form with a plutonium isotopic assay of plutonium-238 of more than 50 % by weight; Note: 1C012.a. does not control: a.
Shipments with a plutonium content of 1 g or less; b.
Shipments of 3 "effective grammes" or less when contained in a sensing component in instruments. b.
"Previously separated" neptunium-237 in any form.
Note: 1C012.b. does not control shipments with a neptunium-237 content of 1 g or less.
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.
Note 1: 1C101 includes: a.
Structural materials and coatings specially designed for reduced radar reflectivity; b.
Coatings, including paints, specially designed for reduced or tailored reflectivity or emissivity in the microwave, infrared or ultraviolet regions of the electromagnetic spectrum.
Note 2: 1C101 does not include coatings when specially used for the thermal control of satellites.
Technical Note: In 1C101 ‘missile’ means complete rocket systems and unmanned aerial vehicle systems capable of a range exceeding 300 km.
1C102
Resaturated pyrolised carbon-carbon materials designed for space launch vehicles specified in 9A004 or sounding rockets specified in 9A104.