Pressure effects on the pump-fed Liquid Rocket Booster (LRB) of the Space Transportation System are examined. Results from the buckling tests; bending moments tests; barrel, propellant tanks, frame XB1513, nose cone, and intertank tests; and finite element examination of forward and aft skirts are presented.


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    Title :

    Liquid Rocket Booster (LRB) for the Space Transportation System (STS) Systems Study. Appendix A: Stress Analysis Report for the Pump-Fed and Pressure-Fed Liquid Rocket Booster


    Publication date :

    1989


    Size :

    56 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English