Investigation of integrated aerobraking spacecraft and associated technology implications in order to evaluate advantages and disadvantages of this mode; included are parameter and conceptual design studies to define spacecraft weights and their sensitivity to variations in environmental models assumed, crew size, mission profile, propellants, etc, as well as internal packaging arrangements; secondary objective was to analyze requirements for system simulation, testing, and qualification. (15691)


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    Title :

    Study of technology requirements for atmosphere braking to orbit about mars and venus


    Additional title:

    NASA CR


    Contributors:
    Repic, E.M. (author)

    Published in:

    Publication date :

    1968


    Size :

    23 pages


    Type of media :

    Report


    Type of material :

    Print


    Language :

    English


    Keywords :