Throttling of rocket propulsion systems represents means for obtaining precise control of ballistic missile and space vehicle flight characteristics, and for enabling single rocket engine to accommodate propulsive requirements of different maneuvers; review of principal mission areas in which throttling is required and summary of major throttling techniques.


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    Titel :

    Toward variable-thrust liquid-rocket engine


    Weitere Titelangaben:

    Astronautics Aerospace Eng


    Beteiligte:
    Welton, D.E. (Autor:in) / Bensky, S.M. (Autor:in) / Hiland, J.R. (Autor:in)


    Erscheinungsdatum :

    1963


    Format / Umfang :

    5 pages


    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :



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    Variable Thrust Rocket Engines

    Bollinger, Loren E. / Lemmon, Jr. Alexis W. / Goldsmith, Martin | AIAA | 1960



    Britain's first variable-thrust rocket

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