The NASA manned space station will consist of three main elements: habitable modules, solar collectors, and their interconnecting hardware. The most arduous of the requirements to be met by this configuration is the simultaneous integration of terrestrial, solar, and celestial viewing instruments, since omnidirectional simultaneous viewing is made difficult by the station's large solar energy collection devices. The space station also imposes unique design conditions on individual subsystems, such as the power distribution and energy storage hardware. In particular, the thermal control subsystem must be designed to meet a variety of mission, payload, and housekeeping tasks that demand a large heat rejection capacity. Novel environmental control and life support subsystem technology will be indispensable.


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    Titel :

    Space station design - Innovation and compromise


    Beteiligte:
    Powell, L. E. (Autor:in) / Cohen, A. (Autor:in) / Craig, M. (Autor:in)

    Erschienen in:

    Erscheinungsdatum :

    01.09.1984



    Medientyp :

    Sonstige


    Format :

    Keine Angabe


    Sprache :

    Englisch


    Schlagwörter :


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    Engineering and design - optimisation by compromise

    Fuegener,L. / Hochschule Pforzheim,DE | Kraftfahrwesen


    Space station design

    Berglund, R. A. / Heberlig, J. C. | NTRS | 1970


    Space Station Design

    Heberlig, Jack C. / Berglund, Rene A. | SAE Technical Papers | 1970