Document ID: chunk:federal_register_of_legislation:F2024L01024:front:0:p246
Version: federal_register_of_legislation:F2024L01024
Segment Type: other
Provision Reference: 
Character Range: 700672–703553

wave (e.g., a sine wave) and systems capable of generating a broad band random vibration (i.e., power spectrum).
                  2. In 9B106.a.2., 'designed or modified' means the environmental chamber provides appropriate interfaces (e.g., sealing devices) to incorporate a shaker unit or other vibration test equipment as specified by 2B116.
                  3. In 9B106.a.2. 'bare table' means a flat table, or surface, with no fixture or fittings.
b. Environmental chambers capable of simulating the following flight conditions:
1. Acoustic environments at an overall sound pressure level of 140 dB or greater (referenced to 20 µPa) or with a total rated acoustic power output of 4 kW or greater; and
2. Altitude equal to or greater than 15 km; or
3. Temperature range from below 223 K (‑50oC) to above 398 K (+125oC).
9. B. 107. 'Aerothermodynamic test facilities', usable for 'missiles' or their subsystems, having any of the following characteristics:
a. an electrical power supply equal to or greater than 5 MW; or
b. a gas supply total pressure equal to or greater than 3 MPa.
Technical notes:
1. In 9B107 'missile' means complete rocket systems capable of a range exceeding 300km.
2. In 9B107 'aerothermodynamic test facilities' include plasma arc jet facilities and plasma wind tunnels for the study of thermal and mechanical effects of airflow on objects.
9. B. 115. Specially designed "production equipment" for the systems, sub‑systems and components specified by 9A005 to 9A009, 9A011, 9A101, 9A102, 9A105 to 9A109, 9A111, 9A116 to 9A120.
9. B. 116. Specially designed "production facilities" for the space launch vehicles specified by 9A004, or systems, sub‑systems, and components specified by 9A005 to 9A009, 9A011, 9A101, 9A102, 9A104 to 9A109, 9A111, 9A116 to 9A120, or complete rocket systems or "unmanned aerial vehicles" capable of a range exceeding 300 km.
9. B. 117. 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 68 kN of thrust; or
b. Capable of simultaneously measuring the three axial thrust components.
9. C.  Materials
9. C. 108. "Insulation" material in bulk form and "interior lining", other than those specified by 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.
9. C. 110. Resin impregnated fibre prepregs and metal coated fibre preforms therefor, for composite structures, laminates and manufactures specified by 9A110, made either with organic matrix or metal matrix utilising fibrous or filamentary reinforcements having a "specific tensile strength" greater than 7.62 x 104 m and a "specific modulus" greater than 3.18 x 106 m.
N.B.: SEE