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Characteristics of Subcooled Liquid Methane During Passage Through a Spray-Bar Joule-Thompson Thermodynamic Vent SystemNASA s Marshall Space Flight Center (MSFC) conducted liquid methane (LCH4) testing in November 2006 using the multipurpose hydrogen test bed (MHTB) outfitted with a spray-bar thermodynamic vent system (TVS). The basic objective was to identify any unusual or unique thermodynamic characteristics associated with subcooled LCH4 that should be considered in the design of space-based TVSs. Thirteen days of testing were performed with total tank heat loads ranging from 720 W to 420 W at a fill level of approximately 90%. During an updated evaluation of the data, it was noted that as the fluid passed through the Joule Thompson expansion, thermodynamic conditions consistent with the pervasive presence of metastability were indicated. This paper describes the observed thermodynamic conditions that correspond with metastability and effects on TVS performance.
Document ID
20110015844
Acquisition Source
Marshall Space Flight Center
Document Type
Conference Paper
Authors
Hastings, L. J.
(Alpha Technology Huntsville, AL, United States)
Bolshinskiy, L. G.
(Alabama Univ. Huntsville, AL, United States)
Hedayat, A.
(NASA Marshall Space Flight Center Huntsville, AL, United States)
Schnell, A.
(NASA Marshall Space Flight Center Huntsville, AL, United States)
Date Acquired
August 25, 2013
Publication Date
June 8, 2011
Subject Category
Propellants And Fuels
Report/Patent Number
M11-1003
Meeting Information
Meeting: 24th Space Cryogenics Workshop 2011
Location: Coeur d''Alene, ID
Country: United States
Start Date: June 8, 2011
End Date: June 10, 2011
Sponsors: Cryogenic Society of America, Inc.
Distribution Limits
Public
Copyright
Public Use Permitted.
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