NASA NTRS · 19650046054
Designing for compatibility in high-performance lp engines.
Abstract
Quantitative design criteria for priori injector designs yielding combustion process compatible with thrust chamber-nozzle materials
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Evans, D. D., Rupe, J. H.. 1965-06-01. Designing for compatibility in high-performance lp engines.. https://ntrs.nasa.gov/citations/19650046054
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