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No-vent fill pressurization tests using a cryogen simulantThe results are described of an experimental program which studied the performance of various no-vent fill techniques for tank-to-tank liquid transfer. The tests were performed using a cryogen simulant (Freon-114) and a test bed consisting of a multiple tank/plumbing network that enabled studies of a variety of different inlet flow and active mixing regimes. Several results and conclusions were drawn from the 26 transfer experiments comprising the program. Most notable was the significant improvement in fill performance (i.e., minimized fill time and maximized fill fraction) with increased agitation of the liquid surface. Another was the close correlation between measured condensation rates and those predicted by recent theories which express condensation as a function of turbulent eddy effects on the liquid surface. In most cases, test data exhibited strong agreement with an analytical model which accounts for tank heat transfer and thermodynamics in a 1 g environment.
Document ID
19920066094
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Schmidt, G.
(NASA Marshall Space Flight Center Huntsville, AL, United States)
Carrigan, R.
(NASA Marshall Space Flight Center Huntsville, AL, United States)
Hahs, J.
(NASA Marshall Space Flight Center Huntsville, AL, United States)
Vaughan, D.
(NASA Marshall Space Flight Center Huntsville, AL, United States)
Foust, D.
(Martin Marietta Space Systems Huntsville, AL, United States)
Date Acquired
August 15, 2013
Publication Date
July 1, 1992
Subject Category
Fluid Mechanics And Heat Transfer
Report/Patent Number
AIAA PAPER 92-3062
Accession Number
92A48718
Distribution Limits
Public
Copyright
Other

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