The performance requirements, preliminary designs, and development program plans for an airborne recovery system for the space shuttle solid rocket booster are discussed. The analyses performed during the study phase of the program are presented. The basic considerations which established the system configuration are defined. A Monte Carlo statistical technique using random sampling of the probability distribution for the critical water impact parameters was used to determine the failure probability of each solid rocket booster component as functions of impact velocity and component strength capability.
Space shuttle solid rocket booster recovery system definition, volume 1
1973-10-01
Report
No indication
English
Space shuttle solid rocket booster recovery subsystem
NTRS | 1981
|Space Shuttle Solid Rocket Booster Recovery Subsystem
NTIS | 1981
|