SATURN project and development of rocket booster by Rocketdyne, having thrust uprating of 188,000 lb to develop 8-engine cluster thrust of over 1.5 million lb; propellant combination is liquid oxygen and RP-1; H-1 Model employs thrust chamber, turbopump assembly, gas generator system, and control valves developed in IRBM and ICBM programs; thrust buildup characteristics; thrust chamber assembly; engine control; clustering effects; feasibility study of recovering booster after flight.
H-1 rocket engine for saturn
SAE -- Paper
SAE Meeting ; 1960 Boosters
1960
9 pages
Conference paper
English
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