Space system consists of boosters, transfer stage, and spacecraft vehicle required to perform mission after injection into desired trajectory; procedure required in sizing and configuration study of space vehicle is described and factors which must be considered such as aerodynamic, power plant, and other loads; material selection, design of space cabins, propellant tank design and common bulkhead or dome between two vessels are also considered.


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    Titel :

    Space technology -- Spacecraft systems


    Weitere Titelangaben:

    NASA SP


    Beteiligte:
    Abraham, L.H. (Autor:in)


    Erscheinungsdatum :

    1965


    Format / Umfang :

    85 pages


    Medientyp :

    Report


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :