SATURN project and development of rocket booster by Rocketdyne, having thrust uprating of 188,000 lb to develop 8-engine cluster thrust of over 1.5 million lb; propellant combination is liquid oxygen and RP-1; H-1 Model employs thrust chamber, turbopump assembly, gas generator system, and control valves developed in IRBM and ICBM programs; thrust buildup characteristics; thrust chamber assembly; engine control; clustering effects; feasibility study of recovering booster after flight.


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    Titel :

    H-1 rocket engine for saturn


    Weitere Titelangaben:

    SAE -- Paper


    Beteiligte:
    Healy, R. (Autor:in)

    Kongress:

    SAE Meeting ; 1960 Boosters



    Erscheinungsdatum :

    1960


    Format / Umfang :

    9 pages


    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :


    THE H-l ROCKET ENGINE FOR SATURN

    HEALY, ROY | SAE Technical Papers | 1960





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    Reichl, Eugen | SLUB | 2018