Hardware considerations and the orbital flight test program of the Space Shuttle are discussed, including reference to the Space Shuttle main engine, payload bay doors, TV cameras for flight inspection, and launch crew escape schemes. Particular attention is given to the thermal protection system consisting of 32,000 tiles composed of approximately 3% pure silica fibers and 97% air, which has a design requirement of keeping the basic aluminum skin below 350 F for a surface temperature of 2700 F.


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen


    Exportieren, teilen und zitieren



    Titel :

    Space Shuttle status


    Beteiligte:
    Slayton, D. K. (Autor:in)

    Erscheinungsdatum :

    01.01.1979


    Medientyp :

    Sonstige


    Format :

    Keine Angabe


    Sprache :

    Englisch


    Schlagwörter :


    Space shuttle status

    Slayton, D. K. | NTRS | 1980


    Space Shuttle redesign status

    Brand, Vance D. | NTRS | 1986


    Space Shuttle status report.

    Peil, N. G. | NTRS | 1973


    Space Shuttle Transition Management Status

    Henderson, Edward / Norbraten, Gordon | AIAA | 2008