Objective of Project Nimbus is to provide capability for continuous satellite observation for application to weather analyses and forecasting; details of fundamental criteria and conditions that formed basis for Nimbus spacecraft design, characteristics of spacecraft and its major subsystems; selection of solar power; silicon cell surface area of 44 sq ft is available and intercepts 5700 w of solar energy during sun illumination; telemetry, sensory systems, high and medium infrared radiometer, ground systems, etc.


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    Titel :

    Nimbus spacecraft system


    Weitere Titelangaben:

    Aerospace Eng


    Beteiligte:
    Stampfl, R. (Autor:in) / Press, H. (Autor:in)

    Erschienen in:

    Erscheinungsdatum :

    1962


    Format / Umfang :

    13 pages


    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :


    NIMBUS SPACECRAFT SYSTEM

    Press, H. / Stampfl, R. | NTRS | 1962


    The nimbus spacecraft system

    Press, H. / Stampfl, R. | NTRS | 1962


    The nimbus spacecraft system

    Press, H. | NTRS | 1964


    Nimbus Spacecraft System Concept

    R. Stampfl | NTRS | 1962


    NIMBUS SPACECRAFT SYSTEM DEVELOPMENT

    Michaels, J. V. | NTRS | 1962