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Optimization of nonequilibrium nozzle performance for selected system considerations.Optimum nonequilibrium nozzle performance for hydrogen-fluorine propellant system, considering contour, engine/nozzle weights and recombination kinetics
Document ID
19690054663
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Bender, L. S.
Burwell, W. G.
Sarli, V. J.
Date Acquired
August 5, 2013
Publication Date
June 1, 1969
Publication Information
Publisher: AMERICAN INST. OF AERONAUTICS AND ASTRONAUTICS,
Subject Category
Aerodynamics
Report/Patent Number
AIAA PAPER 69-472
Report Number: AIAA PAPER 69-472
Meeting Information
Meeting: AMERICAN INST. OF AERONAUTICS AND ASTRONAUTICS, PROPULSION JOINT SPECIALIST CONFERENCE
Location: COLORADO SPRINGS, COLO.
Start Date: June 9, 1969
End Date: June 13, 1969
Sponsors: AMERICAN INST. OF AERONAUTICS AND ASTRONAUTICS
Accession Number
69A32652
Funding Number(s)
CONTRACT_GRANT: NASW-1293
CONTRACT_GRANT: NASW-1293
CONTRACT_GRANT: NAS3-2572
CONTRACT_GRANT: NASW-366
Distribution Limits
Public
Copyright
Other

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