NASA NTRS · 19800006944
Advanced oxygen-hydrocarbon rocket engine study
Abstract
A consistent engine system data base was generated for defining advantages and disadvantages, system performance and operating limits, engine parametric data, and technology requirements for candidate high pressure LO2/HC engine systems. Optimum LO2/HC engine power cycles were synthetized and representative conceptual engine design generated for a specified advanced surface to orbit transportation system.
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Obrien, C. J.. 1979-12-10. Advanced oxygen-hydrocarbon rocket engine study. https://ntrs.nasa.gov/citations/19800006944
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