2.
Altitude equal to or greater than 15 km; or
3.
Temperature range of at least 223 K (- 50 °C) to 398 K (+125 °C).
I.9A.022
ex 9B115
Specially designed "production equipment" for the systems, sub-systems and components specified in I.9A.002, I.9A.004, I.9A.006 to I.9A.010, I.9A.012, I.9A.014 to I.9A.017
I.9A.023
ex 9B116
Specially designed "production facilities" for the space launch vehicles specified in I.9A.001, or systems, sub-systems, and components specified in I.9A.002, I.9A.004, I.9A.005 to I.9A.010, I.9A.012, or I.9A.014 to I.9A.017.
N.B.: See also Military Goods Controls for "production facilities" for rockets and missiles.
I.9A.024
ex 9B117*
Test benches and test stands for solid or liquid propellant rockets or rocket motors, having either of the following characteristics:
a.*
The capacity to handle more than 90 kN of thrust; or
b.
Capable of simultaneously measuring the three axial thrust components.
I.9A.025
9C108
"Insulation" material in bulk form and "interior lining", for rocket motor cases usable in "missiles" or specially designed for 'missiles'.
Technical Note:
In I.9A.025 'missile' means complete rocket systems and unmanned aerial vehicle systems capable of a range exceeding 300 km.
I.9A.026
9C110
Resin impregnated fibre prepregs and metal coated fibre preforms therefor, for composite structures, laminates and manufactures specified in I.9A.011, 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.
N.B.: See also I.1A.024 and I.1A.034.
Note: The only resin impregnated fibre prepregs specified in entry I.9A.026 are those using resins with a glass transition temperature (Tg), after cure, exceeding 418 K (145 °C) as determined by ASTM D4065 or equivalent.
I.9B Technology, including software
No
Relevant item(s) from Annex to Regulation (EC) No 1183/2007
Description
I.9B.001
ex 9D001
"Software" specially designed or modified for the "development" of equipment or "technology" specified in I.9A.002, I.9A.009, I.9A.012, I.9A.015 or I.9A.016.
I.9B.002
9D101
"Software" specially designed or modified for the "use" of goods specified in I.9A.020, I.9A.021, I.9A.023 or I.9A.024.
I.9B.003
9D103
"Software" specially designed for modelling, simulation or design integration of the space launch vehicles specified in I.9A.001 or sounding rockets specified in I.9A.005, or the subsystems specified in I.9A.006.a., I.9A.007, I.9A.009, I.9A.014 or I.9A.017.
Note: "Software" specified in I.9B.003 remains prohibited when combined with specially designed hardware specified in I.4A.003.
I.9B.004
ex 9D104
"Software" specially designed or modified for the "use" of goods specified in 9A005, I.9A.002, I.9A.004, I.9A.006, I.9A.007.c., I.9A.007.d., I.9A.008, I.9A.009.c., I.9A.010, I.9A.012, I.9A.013.a., I.9A.014.d., I.9A.015 or I.9A.016.
I.9B.005
9D105
"Software" which coordinates the function of more than one subsystem, specially designed or modified for "use" in space launch vehicles specified in I.9A.001 or sounding rockets specified in I.9A.005.
I.9B.006
ex 9E001
"Technology" according to the General Technology Note for the "development" of equipment or "software" specified in I.9A.001, I.9A.003, I.9A.021 to I.9A.024, or I.9B.002 to I.9B.005.
I.9B.007
ex 9E002
"Technology" according to the General Technology Note for the "production" of equipment specified in I.9A.001, I.9A.003 or I.9A.021 to I.9A.024.