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Design and demonstrate the performance of cryogenic components representative of space vehicles : Start basket liquid acquisition device performance analysis

Published:
Feb 1, 1987.
Physical Description:
1 electronic document
Online Version

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Unclassified, Unlimited, Publicly available.
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Summary:
The objective was to design, fabricate and test an integrated cryogenic test article incorporating both fluid and thermal propellant management subsystems. A 2.2 m (87 in) diameter aluminum test tank was outfitted with multilayer insulation, helium purge system, low-conductive tank supports, thermodynamic vent system, liquid acquisition device and immersed outflow pump. Tests and analysis performed on the start basket liquid acquisition device and studies of the liquid retention characteristics of fine mesh screens are discussed.
Other Subject(s):
Collection:
NASA Technical Reports Server (NTRS) Collection.
Note:
Document ID: 19870016648.
Accession ID: 87N26081.
NAS 1.26:179138.
NASA-CR-179138.
GDSS-CRAD-87-004.
Terms of Use and Reproduction:
No Copyright.
View MARC record | catkey: 15698167