Thermal insulation requirements of vehicles exposed for extended periods to solar space environment and heat flow paths pertaining to bipropellant liquid propulsion systems; comparison of several high energy propellant combinations is made in terms of payload capability in mission; results show that systems considered can sustain coast periods up to 15,000 hr (2 yr) without significant change in payload magnitudes.


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    Titel :

    High energy propellant comparisons for space missions


    Weitere Titelangaben:

    ARS J


    Beteiligte:
    Burry, R.V. (Autor:in) / Jortner, J. (Autor:in) / Rosemary, J.K. (Autor:in)

    Erschienen in:

    ARS Journal ; 31 , n 5 ; p 609-613


    Erscheinungsdatum :

    1961


    Format / Umfang :

    5 pages


    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :


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