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Pressurization of cryogens: A review of current technology and its applicability to low-gravity conditionsA review of technology, history, and current status for pressurized expulsion of cryogenic tankage is presented. Use of tank pressurization to expel cryogenic fluids will continue to be studied for future spacecraft applications over a range of operating conditions in the low-gravity environment. The review examines experimental test results and analytical model development for quiescent and agitated conditions in normal-gravity, followed by a discussion of pressurization and expulsion in low-gravity. Validated, 1-D, finite difference codes exist for the prediction of pressurant mass requirements within the range of quiescent normal-gravity test data. To date, the effects of liquid sloshing have been characterized by tests in normal-gravity, but analytical models capable of predicting pressurant gas requirements remain unavailable. Efforts to develop multidimensional modeling capabilities in both normal and low-gravity have recently occurred. Low-gravity cryogenic fluid transfer experiments are needed to obtain low-gravity pressurized expulsion data. This data is required to guide analytical model development and to verify code performance.
Document ID
19920020426
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Vandresar, N. T.
(NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
September 6, 2013
Publication Date
July 1, 1992
Subject Category
Propellants And Fuels
Report/Patent Number
AIAA PAPER 92-3061
NAS 1.15:105746
E-7150
NASA-TM-105746
Meeting Information
Meeting: Joint Propulsion Conference and Exhibit
Location: Nashville, TN
Country: United States
Start Date: July 6, 1992
End Date: July 8, 1992
Sponsors: SAE, ASME, ASEE, AIAA
Accession Number
92N29669
Funding Number(s)
PROJECT: RTOP 506-42-73
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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