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)
Investigation of Safe-Life Fail-Safe Criteria for the Space Shuttle
1972
300 pages
Report
Keine Angabe
Englisch
Engineering Index Backfile | 1960
|Factors of Safety and Fail Safe Strength Criteria
NTIS | 1966
|