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Testing and Analytical Modeling for Purging Process of a Cryogenic LineTo gain confidence in developing analytical models of the purging process for the cryogenic main propulsion systems of upper stage, two test series were conducted. The test article, a 3.35 m long with the diameter of 20 cm incline line, was filled with liquid or gaseous hydrogen and then purged with gaseous helium (GHe). Total of 10 tests were conducted. The influences of GHe flow rates and initial temperatures were evaluated. The Generalized Fluid System Simulation Program (GFSSP), an in-house general-purpose fluid system analyzer computer program, was utilized to model and simulate selective tests. The test procedures, modeling descriptions, and the results are presented in the following sections.
Document ID
20150016515
Acquisition Source
Marshall Space Flight Center
Document Type
Conference Paper
Authors
Hedayat, A.
(NASA Marshall Space Flight Center Huntsville, AL, United States)
Mazurkivich, P. V.
(NASA Marshall Space Flight Center Huntsville, AL, United States)
Nelson, M. A.
(NASA Marshall Space Flight Center Huntsville, AL, United States)
Majumdar, A. K.
(NASA Marshall Space Flight Center Huntsville, AL, United States)
Date Acquired
August 27, 2015
Publication Date
June 29, 2015
Subject Category
Propellants And Fuels
Report/Patent Number
M15-4691
Report Number: M15-4691
Meeting Information
Meeting: Cryogenic Engineering Conference
Location: Tucson, AZ
Country: United States
Start Date: June 29, 2015
End Date: July 2, 2015
Sponsors: Cryogenic Society of America, Inc.
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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