Approach is based on Saturn carrier vehicle family; development sequence envisioned starts with Mercury capsule, proceeds to variable lift/drag capsule used as orbital return vehicle, to nonrotating earth-assembled 6- to 10-man laboratory, defined as orbital one-piece satellite; design criteria considered for latter: orbital selection and control, general layout, control systems, crew engineering and life-support systems; equipment and logistic support.


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    Titel :

    Design criteria and their application to economical manned satellites


    Weitere Titelangaben:

    Aero/Space Eng


    Beteiligte:
    Koelle, H.H. (Autor:in) / Engler, E.E. (Autor:in) / Massey, J.W. (Autor:in)

    Erschienen in:

    Erscheinungsdatum :

    1960


    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :


    Preliminary studies of manned satellites

    Faget, Maxime A. / Garland, Benjamine J. / Buglia, James J. | TIBKAT | 1962



    Radiation shielding requirements for manned satellites

    French, F.W. / Hansen, K.F. | Engineering Index Backfile | 1965