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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    Title :

    Toward variable-thrust liquid-rocket engine


    Additional title:

    Astronautics Aerospace Eng


    Contributors:
    Welton, D.E. (author) / Bensky, S.M. (author) / Hiland, J.R. (author)


    Publication date :

    1963


    Size :

    5 pages


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English


    Keywords :



    VARIABLE-THRUST LIQUID PROPELLANT ROCKET ENGINES

    WELTON, D. / BENSKY, M. / HILAND, J. | AIAA | 1963



    Variable Thrust Rocket Engines

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


    Britain's first variable-thrust rocket

    Engineering Index Backfile | 1956