Description of AOSO Mark II configuration which resulted from phase-I design efforts; spacecraft consists of experiment package, spacecraft assembly, and front cover, and can be aimed at sun with precision of plus or minus 5 arc-sec by means of fine sun sensor provided by spacecraft; description of orbital mechanics, experiment integration provisions, stabilization and control subsystem and fine sun sensor, communications and data handling subsystem, and power supply subsystem; tests carried out and development status.


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    Titel :

    Development approach for advanced orbiting solar observatory spacecraft


    Weitere Titelangaben:

    J Spacecraft Rockets


    Beteiligte:
    Evans, W.B. (Autor:in)

    Erschienen in:

    Erscheinungsdatum :

    1966


    Format / Umfang :

    7 pages


    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :