An evaluation is presented of J-2 engine modifications that will simplify operation and improve reliability of the advanced Saturn 1C launch vehicle. Methods of increasing thrust without extensively modifying the S-2 or S-4B stages are also evaluated. A thrust increase was achieved by raising engine combustion through a redesign of the engine thrust chamber and propellant feed system.
Extendible rocket nozzle development
1972-08-01
Miscellaneous
No indication
English
Performance of the aerobell extendible rocket nozzle
AIAA | 1969
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|IUS nozzle and extendible exit cone development
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