Unmanned spacecraft flown on missions to the outer planets of the solar system have included flybys, planetary orbiters, and atmospheric probes during the last three decades. The thermal design, test, and analysis approach applied to these spacecraft evolved from the passive thermal designs applied to the earlier lunar and interplanetary spacecraft. The inflight temperature data from representative sets of engineering subsystems and science instruments from a subset of these spacecraft are compared to those obtained during the ground test programs and from the prelaunch predictions. Several lessons are presented with specific recommendations for considerations for new projects to aid in the planning of cost effective temperature design, test, and analysis programs.


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    Titel :

    Outer planet spacecraft temperature testing and analysis


    Beteiligte:
    Hoffman, A. R. (Autor:in) / Avila, A. (Autor:in)

    Kongress:

    22nd Space Simulation Conference


    Erscheinungsdatum :

    2002-10-24


    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Keine Angabe


    Sprache :

    Englisch




    Outer planet spacecraft temperature testing and analysis

    Hoffman, A. R. / Avila, A. | NTRS | 2002


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    Draper, R. F. / Purdy, W. I. / Cunningham, G. | NTRS | 1975


    The Outer Planet Mariner Spacecraft

    DRAPER, R. / PURDY, W. / CUNNINGHAM, G. | AIAA | 1975


    Communicating with outer-planet spacecraft

    Couvillon, L. A., Jr. / Eyraud, J. P. / Kermode, A. W. et al. | NTRS | 1970


    Structuring the outer-planet spacecraft

    Dawe, R. H. / Fisher, J. G. / Gram, M. B. et al. | NTRS | 1970