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NASA NTRS · 19810014652

Advanced oxygen-hydrocarbon rocket engine study

Abstract

The advantages and disadvantages, system performance and operating limits, engine parametric data, and technology requirements for candidate high pressure LO2/Hydrocarbon engine systems are summarized. These summaries of parametric analysis and design provide a consistent engine system data base. Power balance data were generated for the eleven engine cycles. Engine cycle rating parameters were established and the desired condition and the effect of the parameter on the engine and/or vehicle are described.

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BibTeXRIS

Obrien, C. J., Salkeld, R.. 1980-06-10. Advanced oxygen-hydrocarbon rocket engine study. https://ntrs.nasa.gov/citations/19810014652

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