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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    Title :

    Space technology -- Spacecraft systems


    Additional title:

    NASA SP


    Contributors:


    Publication date :

    1965


    Size :

    85 pages


    Type of media :

    Report


    Type of material :

    Print


    Language :

    English


    Keywords :