Orbital rendezvous operation is separated into distinct steps, termed "launch", "closing", and "docking"; device, assembled at Rand Corp to simulate in-plane response of orbiting space vehicle to applied thrusts, was used to study manned control of orbital rendezvous maneuver; it was found that pilot with appropriate display and controls could direct extreme terminal portion of rendezvous maneuver with precision and flexibility.


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    Titel :

    Orbital rendezvous simulator


    Weitere Titelangaben:

    Astronautical Sciences Rev


    Beteiligte:
    Levin, E. (Autor:in) / Ward, J. (Autor:in)

    Erschienen in:

    Erscheinungsdatum :

    1959


    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :



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