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Thermodynamic Vent System Performance Testing with Subcooled Liquid Methane and Gaseous Helium PressurantDue to its high specific impulse and favorable thermal properties for storage, liquid methane (LCH4) is being considered as a candidate propellant for exploration architectures. In order to gain an -understanding of any unique considerations involving micro-gravity pressure control with LCH4, testing was conducted at the Marshall Space Flight Center using the Multipurpose Hydrogen Test Bed (MHTB) to evaluate the performance of a spray-bar thermodynamic vent system (TVS) with subcooled LCH4 and gaseous helium (GHe) pressurant. Thirteen days of testing were performed in November 2006, with total tank heat leak conditions of about 715 W and 420 W at a fill level of approximately 90%. The TVS system was used to subcool the LCH4 to a liquid saturation pressure of approximately 55.2 kPa before the tank was pressurized with GHe to a total pressure of 165.5 kPa. A total of 23 TVS cycles were completed. The TVS successfully controlled the ullage pressure within a prescribed control band but did not maintain a stable liquid saturation pressure. This was likely. due to a TVS design not optimized for this particular propellant and test conditions, and possibly due to a large artificially induced heat input directly into the liquid. The capability to reduce liquid saturation pressure as well as maintain it within a prescribed control band, demonstrated that the TVS could be used to seek and maintain a desired liquid inlet temperature for an engine (at a cost of propellant lost through the TVS vent). One special test was conducted at the conclusion of the planned test activities. Reduction of the tank ullage pressure by opening the Joule-Thomson valve (JT) without operating the pump was attempted. The JT remained open for over 9300 seconds, resulting in an ullage pressure reduction of 30 kPa. The special test demonstrated the feasibility of using the JT valve for limited ullage pressure reduction in the event of a pump failure.
Document ID
20090028704
Acquisition Source
Marshall Space Flight Center
Document Type
Conference Paper
Authors
Flachbart, R. H.
(NASA Marshall Space Flight Center Huntsville, AL, United States)
Hastings, L. J.
(Alpha Technology Huntsville, AL, United States)
Hedayat, A.
(NASA Marshall Space Flight Center Huntsville, AL, United States)
Nelson, S. L.
(NASA Marshall Space Flight Center Huntsville, AL, United States)
Tucker, S. P.
(NASA Marshall Space Flight Center Huntsville, AL, United States)
Date Acquired
August 24, 2013
Publication Date
July 11, 2007
Subject Category
Propellants And Fuels
Report/Patent Number
MSFC-328
MSFC-402
Report Number: MSFC-328
Report Number: MSFC-402
Meeting Information
Meeting: Space Cryogenics Workshop
Location: Huntsville, AL
Country: United States
Start Date: July 11, 2007
End Date: July 13, 2007
Sponsors: Cryogenic Society of America, Inc.
Distribution Limits
Public
Copyright
Public Use Permitted.
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