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Liquid Methane Testing With a Large-Scale Spray Bar Thermodynamic Vent SystemNASA's Marshall Space Flight Center conducted liquid methane testing in November 2006 using the multipurpose hydrogen test bed outfitted with a spray bar thermodynamic vent system (TVS). The basic objective was to identify any unusual or unique thermodynamic characteristics associated with densified methane 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 to 420 W at a fill level of approximately 90%. 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 Technical Publication describes conditions that correspond with metastability and its detrimental effects on TVS performance. The observed conditions were primarily functions of methane densification and helium pressurization; therefore, assurance must be provided that metastable conditions have been circumvented in future applications of thermodynamic venting to in-space methane storage.
Document ID
20140011201
Acquisition Source
Marshall Space Flight Center
Document Type
Technical Publication (TP)
Authors
Hastings, L. J.
(Alpha Technology Huntsville, AL, United States)
Bolshinskiy, L. G.
(Jacobs Technologies Engineering Science Contract Group Huntsville, AL, United States)
Hedayat, A.
(NASA Marshall Space Flight Center Huntsville, AL, United States)
Flachbart, R. H.
(NASA Marshall Space Flight Center Huntsville, AL, United States)
Sisco, J. D.
(NASA Marshall Space Flight Center Huntsville, AL, United States)
Schnell. A. R.
(NASA Marshall Space Flight Center Huntsville, AL, United States)
Date Acquired
August 29, 2014
Publication Date
July 1, 2014
Subject Category
Spacecraft Propulsion And Power
Report/Patent Number
NASA/TP-2014-218197
M-1386
Funding Number(s)
CONTRACT_GRANT: NNM09AA18C
Distribution Limits
Public
Copyright
Public Use Permitted.
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