A series of tests were conducted to support the development of the Orbiter Heat Rejection System. The details of the baseline radiator were defined by designing, fabricating, and testing representative hardware. The tests were performed in the Space Environmental Simulation Laboratory Chamber A. An IR source was used to simulate total solar and infrared environmental loads on the flowing shuttle radiators panel. The thermal and mechanical performance of L tube space radiators and their thermal coating were established.


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen


    Exportieren, teilen und zitieren



    Titel :

    Space Shuttle L-Tube Radiator Testing


    Beteiligte:
    M. A. Phillips (Autor:in)

    Erscheinungsdatum :

    1976


    Format / Umfang :

    175 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch




    Space shuttle L-tube radiator testing

    Phillips, M. A. | NTRS | 1976



    Space shuttle orbiter radiator system

    Williams, J. / French, R. | Tema Archiv | 1977



    Thermal vacuum performance testing of the Space Shuttle Orbiter radiator system

    Behrend, A. F., Jr. / Chandler, G. D. / Howell, H. R. | NTRS | 1980