NASA NTRS · 19800010909
Advanced oxygen-hydrocarbon rocket engine study
Abstract
Preliminary identification and evaluation of promising liquid oxygen/ hydrocarbon (LO2/HC) rocket engine cycles is reported. A consistent and reliable data base for vehicle optimization and design studies, to demonstrate the significance of propulsion system improvements, and to select the critical technology areas necessary to realize such advances is presented.
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Obrien, C. J.. 1980-02-11. Advanced oxygen-hydrocarbon rocket engine study. https://ntrs.nasa.gov/citations/19800010909
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