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The COLD-SAT Experiment for Cryogenic Fluid Management TechnologyFuture national space transportation missions will depend on the use of cryogenic fluid management technology development needs for these missions. In-space testing will be conducted in order to show low gravity cryogenic fluid management concepts and to acquire a technical data base. Liquid H2 is the preferred test fluid due to its propellant use. The design of COLD-SAT (Cryogenic On-orbit Liquid Depot Storage, Acquisition, and Transfer Satellite), an Expendable Launch Vehicle (ELV) launched orbital spacecraft that will perform subcritical liquid H2 storage and transfer experiments under low gravity conditions is studied. An Atlas launch vehicle will place COLD-SAT into a circular orbit, and the 3-axis controlled spacecraft bus will provide electric power, experiment control, and data management, attitude control, and propulsive accelerations for the experiments. Low levels of acceleration will provide data on the effects that low gravity might have on the heat and mass transfer processes used. The experiment module will contain 3 liquid H2 tanks; fluid transfer, pressurization and venting equipment; and instrumentation.
Document ID
19910014950
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Schuster, J. R.
(General Dynamics Corp. San Diego, CA, United States)
Wachter, J. P.
(Ford Aerospace and Communications Corp. Palo Alto, CA, United States)
Vento, D. M.
(NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
September 6, 2013
Publication Date
October 1, 1990
Publication Information
Publication: Johns Hopkins Univ., The 1990 JANNAF Propulsion Meeting, Volume 2
Subject Category
Propellants And Fuels
Accession Number
91N24263
Funding Number(s)
CONTRACT_GRANT: NAS3-25062
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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