The results of the sequence of tests performed on the space shuttle solid rocket booster thrust vector control subsystem are presented. The operational characteristics of the thrust vector control subsystem components, as determined from the tests, are discussed. Special analyses of fuel consumption, basic steady state characteristics, GN2 spin, and actuator displacement were reviewed which will aid in understanding the performance of the auxiliary power unit. The possibility of components malfunction is also discussed.


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    Title :

    Solid rocket booster thrust vector control subsystem test report (D-1)


    Contributors:
    Pagan, B. (author)

    Publication date :

    1978-04-01


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English