A standard spacecraft bus compatible with NASA launch vehicles, including STS, for four reference missions (Sun, Earth, stellar pointing from low Earth orbit, Earth pointing from geostationary orbit) was designed. The modular serviceable design stems from its use of passive acme screws for module attachment and scoop proof electrical connectors for electrical interfaces. A flight support system includes command and telemetry links.


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    Title :

    Multimission Modular Spacecraft (MMS). A Serviceable Design Spacecraft


    Contributors:

    Publication date :

    1987


    Size :

    4 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English




    Multimission modular spacecraft (MMS)

    FALKENHAYN, JR., EDWARD | AIAA | 1988





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    Cosme, R. / Lokerson, D. | Tema Archive | 1975