Annex I - VERTIC

▼M2
1C107 (continued)
c. Ceramic composite materials (dielectric constant less than 6 at
any frequency from 100 MHz to 100 GHz) for use in radomes
usable in ‘missiles’, space launch vehicles specified in 9A004
or sounding rockets specified in 9A104;
d. Bulk machinable silicon-carbide reinforced unfired ceramic,
usable for nose tips usable in ‘missiles’, space launch
vehicles specified in 9A004 or sounding rockets specified in
9A104;
e. Reinforced silicon-carbide ceramic composites, usable for nose
tips, reentry vehicles and nozzle flaps usable in ‘missiles’,
space launch vehicles specified in 9A004 or sounding rockets
specified in 9A104.
1C111 Propellants and constituent chemicals for propellants, other than
those specified in 1C011, as follows:
a. Propulsive substances:
1. Spherical aluminium powder, other than that specified in the
Military Goods Controls, with particles of uniform diameter
of less than 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
2591:1988 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).
2. Metal fuels, other than that specified in the Military Goods
Controls, in particle sizes of less than 60 μm, whether
spherical, atomised, spheroidal, flaked or ground, consisting
97 % by weight or more of any of the following:
a. Zirconium;
b. Beryllium;
c. Magnesium; or
d. Alloys of the metals specified in a. to c. above;
Technical Note:
The natural content of hafnium in the zirconium (typically
2 % to 7 %) is counted with the zirconium.
3. Oxidiser substances usable in liquid propellant rocket
engines as follows:
a. Dinitrogen trioxide (CAS 10544-73-7);
b. Nitrogen dioxide (CAS 10102-44-0)/dinitrogen tetroxide
(CAS 10544-72-6);
c. Dinitrogen pentoxide (CAS 10102-03-1);
d. Mixed Oxides of Nitrogen (MON);
2009R0428 — EN — 15.06.2012 — 002.001 — 88