NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Press Enter or click the Search button to begin your search.

Back to Results
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
20140000661
Acquisition Source
Marshall Space Flight Center
Document Type
Abstract
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
February 11, 2014
Publication Date
June 17, 2013
Subject Category
Propellants And Fuels
Report/Patent Number
Report Number: M13-2728
M13-2728
Meeting Information
Meeting: Cryogenic Engineering Conference
Location: Anchorage, AK
Country: United States
Start Date: June 17, 2013
End Date: June 21, 2013
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
No Preview Available