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Numerical Modeling of Thermal Stratification in Cryogenic Propellant TanksComputational Fluid Dynamics (CFD) analysis is performed to investigate liquid blockage in the helium pressure line associated with the propellant (MMH) tank. If a certain amount of propellant is trapped within the helium pressure line, the question is whether the given amount of helium that is available can provide a clear helium flow path with no adverse consequences such as over pressurization of the pressure line.
Document ID
20190000490
Acquisition Source
Glenn Research Center
Document Type
Presentation
Authors
Wang, Xiao-Yen
(NASA Glenn Research Center Cleveland, OH, United States)
Harrison, Jonathan
(Gamma Technologies, LLC. Westmont, IL, United States)
Noonan, Andy
(Gamma Technologies, LLC. Westmont, IL, United States)
Desai, Pooja S.
(NASA Johnson Space Center Houston, TX, United States)
Date Acquired
February 9, 2019
Publication Date
August 20, 2018
Subject Category
Fluid Mechanics And Thermodynamics
Report/Patent Number
GRC-E-DAA-TN60294
Meeting Information
Meeting: Thermal and Fluids Analysis Workshop (TFAWS)
Location: Galveston, TX
Country: United States
Start Date: August 20, 2018
End Date: August 24, 2018
Sponsors: NASA Johnson Space Center
Funding Number(s)
WBS: WBS 448887.05.03.03
Distribution Limits
Public
Copyright
Public Use Permitted.
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