Two Space Shuttle solid propellant rocket motor (SRM) nozzles have been tested, both successfully. This paper summarizes the results of these tests. The SRM nozzle was designed and fabricated at the Wasatch Division of Thiokol Corporation. It is over 13 ft long, has a 54.43 in. initial throat diameter, and weighs over 11 tons. A flex bearing is employed for thrust vector control. Design and acceptance testing summaries are presented, along with the post-test results, erosion and actuation data. (Kursetz)


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    Title :

    Space shuttle nozzle development


    Additional title:

    Entwicklung des Duesensystems fuer den Antrieb der Raumfaehre


    Contributors:

    Published in:

    Publication date :

    1978


    Size :

    8 Seiten, 23 Bilder, 4 Tabellen


    Type of media :

    Conference paper


    Type of material :

    Print


    Language :

    English




    Space Shuttle nozzle review

    CANFIELD, A. / ANDERSON, E. / NICHOLS, G. | AIAA | 1978