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Cryogenic fluid management experimentThe cryogenic fluid management experiment (CFME), designed to characterize subcritical liquid hydrogen storage and expulsion in the low-q space environment, is discussed. The experiment utilizes a fine mesh screen fluid management device to accomplish gas-free liquid expulsion and a thermodynamic vent system to intercept heat leak and control tank pressure. The experiment design evolved from a single flight prototype to provision for a multimission (up to 7) capability. A detailed design of the CFME, a dynamic test article, and dedicated ground support equipment were generated. All materials and parts were identified, and components were selected and specifications prepared. Long lead titanium pressurant spheres and the flight tape recorder and ground reproduce unit were procured. Experiment integration with the shuttle orbiter, Spacelab, and KSC ground operations was coordinated with the appropriate NASA centers, and experiment interfaces were defined. Phase 1 ground and flight safety reviews were conducted. Costs were estimated for fabrication and assembly of the CFME, which will become the storage and supply tank for a cryogenic fluid management facility to investigate fluid management in space.
Document ID
19820007244
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Eberhardt, R. N.
(Martin Marietta Corp. Bethesda, MD, United States)
Bailey, W. J.
(Martin Marietta Corp. Bethesda, MD, United States)
Fester, D. A.
(Martin Marietta Corp. Bethesda, MD, United States)
Date Acquired
September 4, 2013
Publication Date
October 1, 1981
Subject Category
Spacecraft Design, Testing And Performance
Report/Patent Number
NASA-CR-165495
MCR-81-597
Report Number: NASA-CR-165495
Report Number: MCR-81-597
Accession Number
82N15117
Funding Number(s)
CONTRACT_GRANT: NAS3-21591
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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