The development and integration of 16 payload bay liner filters into the existing shuttle/payload contamination evaluation (SPACE) computer program is discussed as well as an initial mission profile model. As part of the mission profile model, a thermal conversion program, a temperature cycling routine, a flexible plot routine and a mission simulation of orbital flight test 3 are presented.


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    Title :

    Orbiter/Payload Contamination Control Assessment Support


    Contributors:

    Publication date :

    1978


    Size :

    110 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English




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    Rantanen, R. O. / Ress, E. B. | NTRS | 1975


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    Orbiter/Payload Contamination Control Assessment Support

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    Payload/Orbiter Contamination Control Assessment Support

    R. O. Rantanen / E. B. Ress | NTIS | 1975