Space launch vehicle begins with a basic propulsion stage, and serves as a missile or small launch vehicle; many are traceable to the 1945 German A-4. Increasing stage size, and increasingly energetic propulsion allows for heavier payloads and greater. Earth to Orbit lift capability. Liquid rocket propulsion began with use of storable (UDMH/N2O4) and evolved to high performing cryogenics (LOX/RP, and LOX/LH). Growth versions of SLV's rely on strap-on propulsive stages of either solid propellants or liquid propellants.


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    Titel :

    Worldwide Space Launch Vehicles and Their Mainstage Liquid Rocket Propulsion


    Beteiligte:

    Kongress:

    AIAA Greater New Orleans Section Meeting ; 2010 ; New Orleans, LA, United States


    Erscheinungsdatum :

    2010-04-13


    Medientyp :

    Sonstige


    Format :

    Keine Angabe


    Sprache :

    Englisch





    FESTIP Technology Developments in Liquid Rocket Propulsion for Reusable Launch Vehicles

    Immich, H. / Caporicci, M. / American Institute of Aeronautics and Astronautics et al. | British Library Conference Proceedings | 1996