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Proposed mechanistic model to simulate transfer line cool-down process using liquid heliumThis paper proposes a mathematical model to simulate the cool-down behavior of a warm transfer line using liquid helium (including He II) in a microgravity environment. The thermal-hydraulic characteristics of different possible flow regimes which may occur during the cool-down process are discussed. Correlations for predicting the heat and momentum transfer rates in each flow regime are presented.
Document ID
19870047181
Acquisition Source
Legacy CDMS
Document Type
Reprint (Version printed in journal)
Authors
Ng, Y. S.
(NASA Ames Research Center Moffett Field, CA, United States)
Lee, J. H.
(NASA Ames Research Center Moffett Field, CA, United States)
Kittel, P.
(NASA Ames Research Center Moffett Field, CA, United States)
Date Acquired
August 13, 2013
Publication Date
April 1, 1987
Publication Information
Publication: Journal of Spacecraft and Rockets
Volume: 24
ISSN: 0022-4650
Subject Category
Engineering (General)
Report/Patent Number
AIAA PAPER 85-0961
Report Number: AIAA PAPER 85-0961
ISSN: 0022-4650
Accession Number
87A34455
Distribution Limits
Public
Copyright
Other

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