A test is described which demonstrates the compatibility of the Skylab Rescue Space Vehicle systems, the ground support equipment, and off-site support facilities by proceeding through a simulated launch countdown, liftoff, and flight. The functions of propellant loading, umbilical ejection, holddown arm release, service arm retraction, liftoff, and inflight separation are simulated. An external power source supplies transfer power to internal, and instrument unit commands are simulated by the digital command system. The test outline is presented along with a list of references, intercommunications information, radio frequency matrix, and interface control chart.


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    Title :

    Skylab Rescue Space Vehicle OAT No. 1 Plugs in Test


    Contributors:

    Publication date :

    1973-06-15


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English


    Keywords :