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Extendible rocket nozzle developmentAn 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.
Document ID
19730004122
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Pryor, D. (NASA Marshall Space Flight Center Huntsville, AL, United States)
Date Acquired
August 7, 2013
Publication Date
August 1, 1972
Publication Information
Publication: Res. Achievements Rev., Vol. 4, No. 6
Subject Category
Propulsion Systems
Accession Number
73N12849
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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IDRelationTitle19730004113Collected WorksResearch Achievements Review, volume 4, no. 6: Chemical propulsion research at MSFC
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