The thermal environment of the Space Shuttle payload bay during the on-orbit phase of the STS flights is presented. The STS Thermal Flight Instrumentation System and various substructures of the Orbiter and the payload are described, as well as the various on-orbit attitudes encountered in the STS flights (the tail to sun, nose to sun, payload bay to sun, etc.). Included are the temperature profiles obtained during the on-orbit STS 1-5 flights (with the payload bay door open), recorded in various substructures of the Orbiter's midsection at different flight attitudes, as well as schematic illustrations of the Space Shuttle system, a typical mission profile, and the Orbiter's substructures.


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    Titel :

    Thermal environments for Space Shuttle payloads


    Beteiligte:
    Fu, J. H. (Autor:in) / Graves, G. R. (Autor:in)

    Erscheinungsdatum :

    01.01.1985


    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Keine Angabe


    Sprache :

    Englisch


    Schlagwörter :


    Thermal environments for Space Shuttle payloads

    FU, J. / GRAVES, G. | AIAA | 1985


    Dynamic environments for space shuttle payloads

    Kern, D. L. / Oconnell, M. R. | NTRS | 1982


    Space science payloads for Shuttle

    French, J. R. | NTRS | 1982


    Venting of Space-Shuttle payloads

    MIRONER, A. / REGAN, F. | AIAA | 1983


    Space Shuttle payloads - An overview

    EDGECOMBE, D. / TURNER, D. | AIAA | 1982