Critical phases of flight that define characteristics of recovery system are conditions and requirements between stage separation to re-entry, re-entry, and terminal descent and landing; vehicle considerations that must be investigated in establishing requirements of recovery system are presented; review of programs initiated at NASA Marshall Space Flight Center, to substantiate recovery program for launch vehicles, viz, H-1 engine salt water immersion tests and booster retrieval exercises at sea.
Launch vehicle recovery system requirements
SAE -- Paper
SAE Meeting ; 1962 Recovery
1962
6 pages
Aufsatz (Konferenz)
Englisch
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