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Centaur propellant acquisition system studyA study was performed to determine the desirability of replacing the hydrogen peroxide settling system on the Centaur D-1S with a capillary acquisition system. A comprehensive screening was performed to select the most promising capillary device fluid acquisition, thermal conditioning, and fabrication techniques. Refillable start baskets and bypass feed start tanks were selected for detailed design. Critical analysis areas were settling and refilling, start sequence development with an initially dry boost pump, and cooling the fluid delivered to the boost pump in order to provide necessary net position suction head (NPSH). Design drawings were prepared for the start basket and start tank concepts for both LO2 and LH2 tanks. System comparisons indicated that the start baskets using wicking for thermal conditioning, and thermal subcooling for boost pump NPSH, are the most desirable systems for future development.
Document ID
19750022406
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Blatt, M. H.
(General Dynamics/Convair San Diego, CA, United States)
Walter, M. D.
(General Dynamics/Convair San Diego, CA, United States)
Date Acquired
September 3, 2013
Publication Date
June 1, 1975
Subject Category
Fluid Mechanics And Heat Transfer
Report/Patent Number
CASD-NAS-75-023
NASA-CR-134811
Report Number: CASD-NAS-75-023
Report Number: NASA-CR-134811
Accession Number
75N30479
Funding Number(s)
CONTRACT_GRANT: NAS3-17802
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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