The Thermal Control Surfaces Experiment (TCSE) is the most complex system retrieved after long term space exposure. The TCSE is a microcosm of complex electro-optical payloads being developed and flown. The objective of the TCSE on the LDEF was to determine the effects of the near-Earth orbital environment and the LDEF induced environment on spacecraft thermal control surfaces. The TCSE was a comprehensive experiment that combined in-space measurements with extensive post-flight analyses of thermal control surfaces to determine the effects of exposure to the low Earth orbit space environment. The TCSE was the first space experiment to measure the optical properties of thermal control surfaces the way they are routinely measured in the lab. The performance of the TCSE flight system on the LDEF was excellent.


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    Title :

    Thermal Control Surfaces Experiment Flight System Performance


    Contributors:
    D. R. Wilkes (author) / L. L. Hummer (author) / J. M. Zwiener (author)

    Publication date :

    1992


    Size :

    15 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English




    Thermal control surfaces experiment flight system performance

    Wilkes, Donald R. / Hummer, Leigh L. / Zwiener, James M. | NTRS | 1991


    Thermal Control Surfaces Experiment Flight System Performance

    D. R. Wilkes / L. L. Hummer / J. M. Zwiener | NTIS | 1991


    Thermal control surfaces experiment flight system performance

    Wilkes, Donald R. / Hummer, Leigh L. / Zwiener, James M. | NTRS | 1992


    Thermal control surfaces experiment (SOO69) flight systems performance

    Wilkes, Donald R. / Hummer, Leigh L. | NTRS | 1991