The liquid propellant rocket engine is for manned aircraft and spacecraft. The engine maintains a constant combustion chamber pressure during throttling at high or low altitudes. The engine has a pintle for varying the exhaust throat area which may be inclined to deflect the exhaust gases for steering purposes.


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    Titel :

    Variable Thrust Rocket Engine Incorporating Thrust Vector Control


    Beteiligte:

    Erscheinungsdatum :

    1965


    Format / Umfang :

    1 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch




    Toward variable-thrust liquid-rocket engine

    Welton, D.E. / Bensky, S.M. / Hiland, J.R. | Engineering Index Backfile | 1963





    Variable Thrust Rocket Engines

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