An investigation was made to determine the effects of a pproach and a fail-safe design approach on the space shuttle booster vehicle structure, and to recommend any changes to the structural design criteria. Two configurations of the booster vehicle were considered, one incorporating a delta wing (B-9U configuration) and the other a swept wing (B-16B configuration). Several major structural components of the booster were studied to determine the fatigue life, -safe capabilities of the baseline design. Each component was investigated to determine the practicability of applying a safe-life or fail-safe design philosophy, the changes such design approaches might require, and the impact of these changes on weight, cost, development plans, and performance. (Author)


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    Title :

    Investigation of Safe-Life Fail-Safe Criteria for the Space Shuttle


    Publication date :

    1972


    Size :

    300 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English