Betekenis van:
rocket propulsion

rocket propulsion
Zelfstandig naamwoord
    • reaction propulsion using stored oxygen for combustion; used where there is insufficient atmospheric oxygen

    Hyperoniemen


    Voorbeeldzinnen

    1. Solid rocket propulsion systems having any of the following:
    2. Hybrid rocket propulsion systems with total impulse capacity exceeding 1.1 MNs.
    3. Hybrid rocket propulsion systems with total impulse capacity exceeding 1.1 MNs.
    4. Liquid rocket propulsion systems containing any of the systems or components, specified in 9A006.
    5. Systems and components, specially designed for liquid rocket propulsion systems, as follows:
    6. 9A008.d. Components, as follows, specially designed for solid rocket propulsion systems:
    7. Components, other than those specified in 9A008, usable in "missiles", as follows, specially designed for solid rocket propulsion systems:
    8. Systems and components specially designed for liquid rocket propulsion systems, as follows: N.B.: SEE ALSO 9A106, 9A108 and 9A.120.
    9. Liquid rocket propulsion systems containing any of the systems or components specified in 9A006. N.B.: SEE ALSO 9A105 and 9A119.
    10. Systems or components, other than those specified in 9A006 as follows, specially designed for liquid rocket propulsion systems:
    11. 7E104 "Technology" for the integration of the flight control, guidance, and propulsion data into a flight management system for optimisation of rocket system trajectory.
    12. 9A007.a. Solid rocket propulsion systems, usable for space launch vehicles specified in 9A004 above or sounding rockets specified in 9A104 below, with any of the following:
    13. 7E104 "Technology" for the integration of the flight control, guidance, and propulsion data into a flight management system for optimisation of rocket system trajectory. —
    14. Solid rocket propulsion systems, usable for space launch vehicles specified in 9A004 above or sounding rockets specified in 9A104 below, with any of the following:
    15. 9A106.c. Systems or components, other than those specified in 9A006, usable in "missiles", as follows, specially designed for liquid rocket propulsion systems: