Last Updated: April 11, 2026
Last Updated: April 11, 2026
b. Pyrolytic or fibrous reinforced graphites, usable for rocket nozzles and reentry vehicle nose tips usable in “missiles”, space launch vehicles specified in 9A004 or sounding rockets specified in 9A104; N.B.: See also 0C004
Code
1C107
EU Code
M6C4
Categories
- ANNEX III - CATEGORY 1 — SPECIAL MATERIALS AND RELATED EQUIPMENT
- ANNEX II - List of other goods and technology, including software, referred to in Article 3a
Subcategory
1C - Materials
Prohibited Supply To
IRAuthority
EU
Document
EU Regulation No 267/2012
Notes
- Bulk machinable silicon-carbide reinforced unfired ceramic usable for nose tips usable in systems specified in 1.A. or 19.A.1.;
- 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.
- 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.
- 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.
- 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 × 10-6m (100 μm) or less, usable for rocket nozzles and re-entry vehicle nose tips, which can be machined to any of the following products:a. Cylinders having a diameter of 120 mm or greater and a length of 50 mm or greater;b. Tubes having an inner diameter of 65 mm or greater and a wall thickness of 25 mm or greater and a length of 50 mm or greater; orc. Blocks having a size of 120 mm × 120 mm × 50 mm or greater
Program information
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