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On-orbit cryogenic fluid transferA number of future NASA and DOD missions have been identified that will require, or could benefit from resupply of cryogenic liquids in orbit. The most promising approach for accomplishing cryogenic fluid transfer in the weightlessness environment of space is to use the thermodynamic filling technique. This approach involves initially reducing the receiver tank temperature by using several charge hold vent cycles followed by filling the tank without venting. Martin Marietta Denver Aerospace, under contract to the NASA Lewis Research Center, is currently developing analytical models to describe the on orbit cryogenic fluid transfer process. A detailed design of a shuttle attached experimental facility, which will provide the data necessary to verify the analytical models, is also being performed.
Document ID
19840017685
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Aydelott, J. C.
(NASA Lewis Research Center Cleveland, OH, United States)
Gille, J. P.
(Martin Marietta Aerospace Denver, United States)
Eberhardt, R. N.
(Martin Marietta Aerospace Denver, United States)
Date Acquired
September 4, 2013
Publication Date
January 1, 1984
Subject Category
Space Transportation
Report/Patent Number
E-2139
AIAA PAPER 84-1343
NASA-TM-83688
NAS 1.15:83688
Report Number: E-2139
Report Number: AIAA PAPER 84-1343
Report Number: NASA-TM-83688
Report Number: NAS 1.15:83688
Meeting Information
Meeting: Joint Propulsion Conf.
Location: Cincinnati, OH
Country: United States
Start Date: June 11, 1984
End Date: June 13, 1984
Sponsors: ASME, AIAA, SAE
Accession Number
84N25753
Funding Number(s)
PROJECT: RTOP 542-03-12
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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