NASA NTRS · 19690054663
Optimization of nonequilibrium nozzle performance for selected system considerations.
Abstract
Optimum nonequilibrium nozzle performance for hydrogen-fluorine propellant system, considering contour, engine/nozzle weights and recombination kinetics
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Bender, L. S., Burwell, W. G., Sarli, V. J.. 1969-06-01. Optimization of nonequilibrium nozzle performance for selected system considerations.. https://ntrs.nasa.gov/citations/19690054663
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