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Pressurization of a Flightweight, Liquid Hydrogen Tank: Evaporation and Condensation at a Liquid Vapor InterfaceEvaporation and condensation at a liquidvapor interface is important for long-term, in-space cryogenic propellant storage. Yet the current understanding of interfacial physics does not predict behavior or evaporation condensation rates. The proposed paper will present a physical model, based on the 1-D Heat equation and Schrages equation which demonstrates thin thermal layers at the fluidvapor interface.
Document ID
20170008112
Acquisition Source
Glenn Research Center
Document Type
Presentation
Authors
Stewart, Mark E.
(Vantage Partners, LLC Cleveland, OH, United States)
Date Acquired
August 31, 2017
Publication Date
July 10, 2017
Subject Category
Fluid Mechanics And Thermodynamics
Propellants And Fuels
Report/Patent Number
GRC-E-DAA-TN44250
Meeting Information
Meeting: AIAA/SAE/ASEE Joint Propulsion Conference
Location: Atlanta, GA
Country: United States
Start Date: June 10, 2017
End Date: June 12, 2017
Sponsors: American Society for Engineering Education (ASEE), American Inst. of Aeronautics and Astronautics, Society of Automotive Engineers, Inc.
Funding Number(s)
CONTRACT_GRANT: NNC12BA01B
WBS: WBS 448887.04.03.02
Distribution Limits
Public
Copyright
Public Use Permitted.
Keywords
Cryogenic hydrogen
computer simulation
propellant storage
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