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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    Titel :

    Orbiter/payload contamination control assessment support


    Beteiligte:
    Rantanen, R. O. (Autor:in) / Strange, D. A. (Autor:in) / Hetrick, M. A. (Autor:in)

    Erscheinungsdatum :

    01.02.1978


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch


    Schlagwörter :


    Payload/orbiter contamination control assessment support

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


    Orbiter/Payload Contamination Control Assessment Support

    R. O. Rantanen / D. A. Strange / M. A. Hetrick | NTIS | 1978


    Payload/Orbiter Contamination Control Assessment Support

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


    Orbiter/payload contamination control assessment support

    Rantanen, R. O. / Jensen, D. A. S. | NTRS | 1977


    Orbiter/Payload Contamination Control Assessment Support

    R. O. Rantanen / D. A. Strangejensen | NTIS | 1977