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Design, fabrication, assembly, and test of a liquid hydrogen acquisition subsystemThe development of a cryogenic fluid system to supply liquid hydrogen to a turbopump at flowrates up to 7.5 pounds per second for a period of approximately 5 seconds before refill, is discussed. Refill is accomplished in less than 10 seconds, during which a constant flowrate can be maintained to the pumps. Diagrams are provided to show the configuration of the system. Subsystem acceptance and functional tests, including acquisition subsystem expulsion, pressurization, and refill were performed. The tests included: (1) thermodynamic vent system operation, (2) warm-gas pressurization effects, (3) hydraulic pressure surge effects, (4) screen device operational limitations, (5) feedline vapor control, and (6) two-phase refill.
Document ID
19740026761
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Blackman, J. B.
(McDonnell-Douglas Astronautics Co. Huntington Beach, CA, United States)
Date Acquired
September 3, 2013
Publication Date
May 1, 1974
Subject Category
Machine Elements And Processes
Report/Patent Number
MDC-G5360
NASA-CR-120447
Report Number: MDC-G5360
Report Number: NASA-CR-120447
Accession Number
74N34874
Funding Number(s)
CONTRACT_GRANT: NAS8-27571
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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