Betekenis van:
rocket propellant

Voorbeeldzinnen

1. Liquid propellant rocket engines, as follows:
2. 9A105.a. Liquid propellant rocket engines, as follows:
3. Oxidiser substances usable in liquid propellant rocket engines as follows:
4. Liquid propellant rocket engines, as follows: N.B.: SEE ALSO 9A119.
5. Other ferrocene derivatives usable as rocket propellant burning rate modifiers, other than those specified in the Military Goods Controls.
6. Test benches and test stands for solid or liquid propellant rockets or rocket motors, having either of the following characteristics:
7. 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:
8. 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;
9. 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;
10. 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.
11. Liquid propellant rocket engines usable in "missiles", other than those specified in 9A005, having a total impulse capacity of 1,1 MNs or greater;
12. 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.
13. 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.
14. 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.
15. 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, usable in "missiles", as follows, specially designed for liquid rocket propulsion systems: a. Ablative liners for thrust or combustion chambers;