Betekenis van:
rocket propellant
rocket propellant
Zelfstandig naamwoord
- vloeibaar gas
- an explosive charge that propels a rocket
Synoniemen
Hyperoniemen
rocket propellant
Zelfstandig naamwoord
- stuwstof
- an explosive charge that propels a rocket
Synoniemen
Hyperoniemen
Voorbeeldzinnen
- Liquid propellant rocket engines, as follows:
- 9A105.a. Liquid propellant rocket engines, as follows:
- Oxidiser substances usable in liquid propellant rocket engines as follows:
- Liquid propellant rocket engines, as follows: N.B.: SEE ALSO 9A119.
- Test benches and test stands for solid or liquid propellant rockets or rocket motors, having either of the following characteristics:
- Liquid propellant rocket engines usable in "missiles", other than those specified in 9A005, having a total impulse capacity of 1.1 MNs or greater; except liquid propellant apogee engines designed or modified for satellite applications and having all of the following:
- Liquid propellant rocket engines usable in "missiles", other than those specified in 9A005, having a total impulse capacity of 1,1 MNs or greater;
- Solid propellant rocket engines, usable in complete rocket systems or unmanned air vehicles, capable of a range of 300 km, other than those specified in 9A007, having total impulse capacity of 0,841 MNs or greater.
- Solid propellant rocket engines, usable in complete rocket systems or unmanned aerial vehicles, capable of a range of 300 km, other than those specified in 9A007, having total impulse capacity equal to or greater than 0,841 MNs.
- Liquid propellant rocket engines, usable in complete rocket systems or unmanned air vehicles, capable of a range of 300 km, other than those specified in 9A005 or 9A105.a., having a total impulse capacity of 0,841 MNs or greater.
- Liquid propellant rocket engines usable in "missiles", other than those specified in 9A005, having a total impulse capacity of 1,1 MNs or greater; b. Liquid propellant rocket engines, usable in complete rocket systems or unmanned air vehicles, capable of a range of 300 km, other than those specified in 9A005 or 9A105.a., having a total impulse capacity of 0,841 MNs or greater. 9A106 Systems or components, other than those specified in 9A006, usable in "missiles", as follows, specially designed for liquid rocket propulsion systems: a. Ablative liners for thrust or combustion chambers;
- liquid propellant rocket engines usable in "missiles", other than those specified in 9A005, having a total impulse capacity equal to or greater than 1,1 MNs; b. liquid propellant rocket engines, usable in complete rocket systems or unmanned aerial vehicles, capable of a range of 300 km, other than those specified in 9A005 or 9A105.a., having a total impulse capacity equal to or greater than 0,841 MNs. 9A106 Systems or components, other than those specified in 9A006 as follows, specially designed for liquid rocket propulsion systems: a. ablative liners for thrust or combustion chambers, usable in "missiles", space launch vehicles specified in 9A004 or sounding rockets specified in 9A104;
- liquid propellant injectors with individual orifices of 0,381 mm or smaller in diameter (an area of 1,14 × 10–3 cm2 or smaller for non-circular orifices) and specially designed for liquid rocket engines;
- Liquid propellant rocket engines usable in "missiles", other than those specified in 9A005, having a total impulse capacity equal to or greater than 1,1 MNs; except liquid propellant apogee engines designed or modified for satellite applications and having all of the following: 1.
- Liquid propellant rocket engines, usable in complete rocket systems or unmanned aerial vehicles, capable of a range of 300 km, other than those specified in 9A005 or 9A105.a., having a total impulse capacity equal to or greater than 0,841 MNs.