NASA NTRS · 19730004122
Extendible rocket nozzle development
Abstract
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.
Keep this discovery
Explore connections, maps & timelines
Pryor, D.. 1972-08-01. Extendible rocket nozzle development. https://ntrs.nasa.gov/citations/19730004122
Cite the original work for its findings. Save a collection to share your selection of sources.