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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    Title :

    Orbital storage of cryogenic propellants for rendezvous missions


    Additional title:

    SAE -- Paper


    Contributors:

    Conference:

    SAE Meeting ; 1962 Boosters



    Publication date :

    1962


    Size :

    14 pages


    Type of media :

    Conference paper


    Type of material :

    Print


    Language :

    English


    Keywords :


    Orbital Storage of Cryogenic Propellants for Rendezvous Missions

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



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