Two classes of thermal conditions occur on Mars flyby; there are long periods of nearly steady-state thermal conditions, yet, over seven month flight period, slow variation can become significant; changing operational modes of spacecraft, in vicinity of Earth and Mars, causes relatively short-term transients which define temperature extremes; design philosophy applied for controlling temperature is outlined and main equipment, magnetometer, and solar panels are selected as examples to illustrate approach employed; thermal testing carried out and flight results obtained are summarized.


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    Titel :

    Maintaining thermal control in mariner


    Weitere Titelangaben:

    Astronautics Aeronautics


    Beteiligte:
    Lewis, D.W. (Autor:in)

    Erschienen in:

    Astronautics and Aeronautics ; 3 , n 10 ; p 30-34


    Erscheinungsdatum :

    1965


    Format / Umfang :

    5 pages


    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :





    Mariner 5

    NTRS | 1967


    Temperature control of mariner v spacecraft

    Dumas, L.N. | Engineering Index Backfile | 1968