Paper discusses analyses conducted on realistic orbital launch booster vehicles utilizing cryogenic propellants; effect on design of cryogenic stages of propellant performance, orbital storage period, and space environment is described, as is influence of design variations upon propellant loss rate in orbit of realistic orbital launch boosters; thermal analysis from boost and transition through orbital conditions is presented.


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    Titel :

    Orbital storage of cryogenic propellants for rendezvous missions


    Weitere Titelangaben:

    SAE -- Paper


    Beteiligte:
    Boyles, Jr., R.Q. (Autor:in) / Tatom, J.W. (Autor:in)

    Kongress:

    SAE Meeting ; 1962 Boosters



    Erscheinungsdatum :

    1962


    Format / Umfang :

    14 pages


    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :


    Orbital Storage of Cryogenic Propellants for Rendezvous Missions

    Taton, J. W. / Boyles, R. Q. | SAE Technical Papers | 1962



    Piloted Mars missions using cryogenic and storable propellants

    Striepe, Scott A. / Desai, Prasun N. | NTRS | 1993


    Piloted Mars Missions Using Cryogenic and Storable Propellants

    Striepe, S. A. / Desai, P. N. / American Astronautical Society et al. | British Library Conference Proceedings | 1993