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

    Erscheinungsdatum :

    1982


    Format / Umfang :

    42 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch





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