Implications of operational requirements on systems design, performance, and cost; considerations include safety and comfort, sonic boom, abort, flyback capability, mission parameters, etc; implementation of systems development -- wholesale expenditures or modest evolutionary steps; first new development seen is reusable passenger vehicle to replace Apollo command and service modules; next, improvements in economy and operations of launch vehicle; partially reusable systems appear most promising.


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    Titel :

    Design considerations for orbital transport systems


    Weitere Titelangaben:

    SAE -- Proc


    Beteiligte:
    Fellenz, D.W. (Autor:in) / Akridge, C.M. (Autor:in)

    Kongress:

    Space Technology Conference ; 1967 Reusable


    Erschienen in:

    Erscheinungsdatum :

    1967


    Format / Umfang :

    27 pages


    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :


    Design considerations for orbital transport systems.

    Akridge, C. M. / Fellenz, D. W. | NTRS | 1967


    Design Considerations for Orbital Transport Systems

    Akridge, Charles M. / Fellenz, Dietrich W. | SAE Technical Papers | 1967


    ORBITAL SPACE PLANE DESIGN CONSIDERATIONS

    Schneider, J. / Searcy, J. / Yechout, T. R. et al. | British Library Conference Proceedings | 2005


    Orbital Space Plane Design Considerations

    Schneider, Joshua / Searcy, Jeffery / Yechout, Thomas | AIAA | 2005