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A pressure control analysis of cryogenic storage systemsSelf-pressurization of cryogenic storage tanks due to heat leak through the thermal protection system is examined along with the performance of various pressure control technologies for application in microgravity environments. Methods of pressure control such as fluid mixing, passive thermodynamic venting, and active thermodynamic venting are analyzed using the homogeneous thermodynamic model. Simplified equations suggested may be used to characterize the performance of various pressure control systems and to design space experiments.
Document ID
19910015147
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Lin, C.-S. (Analex Corp. Fairview Park, OH., United States)
Vandresar, N. T. (NASA Lewis Research Center Cleveland, OH, United States)
Hasan, M. M. (NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
September 6, 2013
Publication Date
January 1, 1991
Subject Category
Propellants And Fuels
Report/Patent Number
NASA-TM-104409
NAS 1.15:104409
E-6235
AIAA PAPER 91-2405
Report Number: NASA-TM-104409
Report Number: NAS 1.15:104409
Report Number: E-6235
Report Number: AIAA PAPER 91-2405
Meeting Information
Meeting: Joint Propulsion Conference
Location: Sacramento, CA
Country: United States
Start Date: June 24, 1991
End Date: June 27, 1991
Sponsors: ASME, American Society for Electrical Engineers, AIAA, SAE
Accession Number
91N24460
Funding Number(s)
PROJECT: RTOP 506-48-00
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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