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The cryogenic on-orbit liquid analytical tool (COOLANT) - A computer program for evaluating the thermodynamic performance of orbital cryogen storage facilitiesThe United States plans to establish a permanent manned presence at the Space Station Freedom in low earth orbit (LEO) and then carry out exploration of the solar system from this base. These plans may require orbital cryogenic propellant storage depots. The COOLANT program has been developed to analyze the thermodynamic performance of these depots to support design tradeoff studies. It was developed as part of the Long Term Cryogenic Storage Facility Systems Study for NASA/MSFC. This paper discusses the program structure and capabilities of the COOLANT program. In addition, the results of an analysis of a 200,000 lbm hydrogen/oxygen storage depot tankset using COOLANT are presented.
Document ID
19910036886
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Taylor, W. J.
(Analex Corp. Fairview Park, OH, United States)
Honkonen, S. C.
(Analex Corp. Fairview Park, OH, United States)
Williams, G. E.
(Analex Corp. Fairview Park, OH, United States)
Liggett, M. W.
(General Dynamics Corp. Space Systems Div., San Diego, CA, United States)
Tucker, S. P.
(NASA Marshall Space Flight Center Huntsville, AL, United States)
Date Acquired
August 15, 2013
Publication Date
January 1, 1991
Subject Category
Fluid Mechanics And Heat Transfer
Report/Patent Number
AIAA PAPER 91-0487
Accession Number
91A21509
Distribution Limits
Public
Copyright
Other

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