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.
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
1989
56 pages
Report
No indication
English