NASA NTRS · 19810020618
Advanced oxygen-hydrocarbon rocket engine study
Abstract
Preliminary identification and evaluation of promising LO2/Hydrocarbon rocket engine cycles were used to produce a consistent and reliable data base for vehicle optimization and design studies. cycles G and C were chosen for design analysis. Preliminary design analysis of the heat transfer subsystem was performed to establish major technology requirements.
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Obrien, C. J., Salkeid, R., Mueggenburg, H., Ewen, R. L.. 1980-08-11. Advanced oxygen-hydrocarbon rocket engine study. https://ntrs.nasa.gov/citations/19810020618
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