Preferred techniques for providing abort pressurization and engine feed system net positive suction pressure (NPSP) for low thrust chemical propulsion systems (LTPS) were determined. A representative LTPS vehicle configuration is presented. Analysis tasks include: propellant heating analysis; pressurant requirements for abort propellant dump; and comparative analysis of pressurization techniques and thermal subcoolers.


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    Titel :

    Low-thrust chemical propulsion system propellant expulsion and thermal conditioning study. Executive summary


    Beteiligte:
    Merino, F. (Autor:in) / Wakabayashi, I. (Autor:in) / Pleasant, R. L. (Autor:in) / Hill, M. (Autor:in)

    Erscheinungsdatum :

    01.04.1982


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch





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