Missile 36D was tested at the Sycamore Canyon Captive Test Site, from 28 October 1959 through 9 February 1960. The purpose of the test program was to study missile tank skin strain characteristics during the thrust build-up transient for both wet and dry engine start configurations. (Author)


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    Title :

    Effects of Engine Thrust Transients on XSM-65D Missiles


    Contributors:

    Publication date :

    1960


    Size :

    151 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English





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