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 :

    1978-02-01


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch


    Schlagwörter :


    Orbiter/Payload Contamination Control Assessment Support

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



    Support of the Boeing IUS in the Orbiter payload

    JONES, JR., E. / MUSGROVE, M. / CHURCH, S. et al. | AIAA | 1981


    Space Shuttle Payload Customer Support Tools: Orbiter-in-a-Box

    Barry, M. R. / Institute of Electrical and Electronics Engineers | British Library Conference Proceedings | 2000