Application of existing Rocket-dyne engines to second stage vehicle applications is examined with respect to potential engine start problems associated with low ambient pressure of high altitude; it is shown that existing booster engines as used in Saturn and late model Atlas missiles are directly applicable; with minor modification, earlier models as used in Thor and Jupiter missiles are adaptable to second stage applications.


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    Titel :

    Altitude start capability of existing large liquid propellant rocket engines


    Weitere Titelangaben:

    SAE -- Paper


    Beteiligte:
    Ezell, W.F. (Autor:in)

    Kongress:

    SAE Meeting ; 1960



    Erscheinungsdatum :

    1960


    Format / Umfang :

    15 pages


    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :




    Altitude Testing of Large Liquid Propellant Engines

    B. Maynard / N. Raines | NTIS | 2008


    Liquid-Propellant Rocket Engines

    Greatrix, David R. | Springer Verlag | 2012


    Altitude Testing of Large Liquid Propellant Engines

    Maynard, Bryon T. / Raines, Nickey G. | NTRS | 2010