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Small experiments for the maturation of orbital cryogenic transfer technologiesThe no-vent fill method is a promising approach to handle the problems of low-g venting during propellant transfer. A receiver tank is first cooled to remove thermal energy from the tank wall and the resultant vapor vented overboard. Then nozzles mix the incoming liquid and residual vapor in the tank maintaining a thermodynamic state which allows the tank to fill with liquid without venting. Ground based testing at NASA Lewis Research Center (LeRC) has demonstrated the no-vent fill process and attempted to bound its low-gravity performance. But, low-gravity testing is required to validate the method. As an alternative to using a dedicated spacecraft for validation the authors have formulated several small scale experiments to study no-vent fill in low-g. Cost goals quickly limited the search to two possibilities: a secondary payload on the Space Shuttle, or a small scale sounding rocket experiment. This paper will discuss the key issues of small scale experimentation and present a conceptual design of a sounding rocket experiment with liquid hydrogen for studying the fill process.
Document ID
19930029701
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Chato, David J.
(NASA Lewis Research Center Cleveland, OH, United States)
Taylor, William J.
(NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
August 15, 2013
Publication Date
August 1, 1992
Subject Category
Spacecraft Propulsion And Power
Report/Patent Number
IAF PAPER 92-0777
Accession Number
93A13698
Distribution Limits
Public
Copyright
Other

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