Publication Date:
2019-07-13
Description:
Optimum nonequilibrium nozzle performance for hydrogen-fluorine propellant system, considering contour, engine/nozzle weights and recombination kinetics
Keywords:
AERODYNAMICS
Type:
AIAA PAPER 69-472
,
AMERICAN INST. OF AERONAUTICS AND ASTRONAUTICS, PROPULSION JOINT SPECIALIST CONFERENCE; Jun 09, 1969 - Jun 13, 1969; COLORADO SPRINGS, COLO.
Format:
text
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