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An analysis of two-phase flow in LH sub 2 pumps for O sub 2 /H sub 2 rocket engines.Hydrogen oxygen rocket engine two phase liquid hydrogen pump capability and hydrodynamic design, analyzing constant-quality flow, acoustic effects, compressible flow and cavitation
Document ID
19690054770
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Bissell, W. R.
Winstead, T. W.
Wong, G. S.
Date Acquired
August 5, 2013
Publication Date
June 1, 1969
Publication Information
Publisher: AMERICAN INST. OF AERONAUTICS AND ASTRONAUTICS,
Subject Category
Propulsion Systems
Report/Patent Number
AIAA PAPER 69-549
Report Number: AIAA PAPER 69-549
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
69A32759
Funding Number(s)
CONTRACT_GRANT: NAS8-20324
Distribution Limits
Public
Copyright
Other

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