Spacecraft radiator concepts are presented that relieve attitude restrictions required by the shuttle orbiter space radiator for baseline and extended capability STS missions. Cost effective heat rejection kits are considered which add additional capability in the form of attached spacelab radiators or a deployable radiator module.


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    Titel :

    Augmented Orbiter Heat Rejection Study


    Beteiligte:
    C. W. Hixon (Autor:in)

    Erscheinungsdatum :

    1981


    Format / Umfang :

    132 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch




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