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Capillary acquisition devices for high-performance vehicles: Executive summaryTechnology areas critical to the development of cryogenic capillary devices were studied. Passive cooling of capillary devices was investigated with an analytical and experimental study of wicking flow. Capillary device refilling with settled fluid was studied using an analytical and experimental program that resulted in successful correlation of a versatile computer program with test data. The program was used to predict Centaur D-1S LO2 and LH2 start basket refilling. Comparisons were made between the baseline Centaur D-1S propellant feed system and feed system alternatives including systems using capillary devices. The preferred concepts from the Centaur D-1S study were examined for APOTV and POTV vehicles for delivery and round trip transfer of payloads between LEO and GEO. Mission profiles were determined to provide propellant usage timelines and the payload partials were defined.
Document ID
19800010908
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Blatt, M. H.
(General Dynamics/Convair San Diego, CA, United States)
Bradshaw, R. D.
(General Dynamics/Convair San Diego, CA, United States)
Risberg, J. A.
(General Dynamics/Convair San Diego, CA, United States)
Date Acquired
September 4, 2013
Publication Date
February 1, 1980
Subject Category
Spacecraft Propulsion And Power
Report/Patent Number
NASA-CR-159658
GDC-CRAD-80-003
Report Number: NASA-CR-159658
Report Number: GDC-CRAD-80-003
Accession Number
80N19185
Funding Number(s)
CONTRACT_GRANT: NAS3-20092
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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