Technical studies show major advantages in propulsion system flexibility, simplicity, reliability, and cost effectiveness attained through use of common propellants for all propulsion functions on cryogenic space vehicles; design considerations involved in development of auxiliary propulsion systems using cryogenic propellants and applicability of catalyst and spark igniter units to oxygen-hydrogen thrust chambers for pulse-mode operations are discussed. (31362)


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    Titel :

    Cryogenic auxiliary propulsion systems


    Weitere Titelangaben:

    ASME Aviation Space -- Progress Prospects


    Beteiligte:
    Barber, H.E. (Autor:in)

    Kongress:

    ASME -- Annual Aviation and Space Conference ; 1968 ; United States , Beverly Hills, CA Propulsion systems



    Erscheinungsdatum :

    1968


    Format / Umfang :

    7 pages


    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :


    Satellite auxiliary propulsion systems

    Holcomb, L. B. | NTRS | 1973


    Auxiliary propulsion

    Rosenberg, S. D. | NTRS | 1984


    Auxiliary propulsion

    SCHWEIKLE, J. / STONE, D. | AIAA | 1971


    Cryogenic Propulsion Stage

    D. Jones | NTIS | 2011


    Auxiliary propulsion

    Schweikle, J. D. / Stone, D. F. | NTRS | 1971