The capability of the 25 kW power module to conduct representative missions which include Earth, solar, and stellar observation as well as zero-gravity experiments was assessed. Mission accommodations and related technical characteristics of the various operating modes are summarized. The minimum power module provides a substantial mission support on sortie flights. The addition of an attitude sensor is required for free-flying pointing missions.


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    Title :

    The 25 W Power Module Evolution Study. Part 3: Conceptual Designs for Power Module Evolution. Volume 5: Mission Accommodations


    Publication date :

    1979


    Size :

    216 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English