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Methods of Helium Injection and Removal for Heat Transfer AugmentationWhile augmentation of heat transfer from a test article by helium gas at low pressures is well known, the method is rarely employed during space simulation testing because the test objectives usually involve simulation of an orbital thermal environment. Test objectives of cryogenic optical testing at Marshall Space Flight Center's X-ray Cryogenic Facility (XRCF) have typically not been constrained by orbital environment parameters. As a result, several methods of helium injection have been utilized at the XRCF since 1999 to decrease thermal transition times. A brief synopsis of these injection (and removal) methods including will be presented.
Document ID
20090014778
Acquisition Source
Marshall Space Flight Center
Document Type
Conference Paper
Authors
Haight, Harlan
(NASA Marshall Space Flight Center Huntsville, AL, United States)
Kegley, Jeff
(NASA Marshall Space Flight Center Huntsville, AL, United States)
Bourdreaux, Meghan
(Alabama Univ. AL, United States)
Date Acquired
August 24, 2013
Publication Date
October 20, 2008
Subject Category
Engineering (General)
Report/Patent Number
MSFC-2119
Report Number: MSFC-2119
Meeting Information
Meeting: 25th Space Simulation Conference
Location: Annapolis, MD
Country: United States
Start Date: October 20, 2008
End Date: October 23, 2008
Distribution Limits
Public
Copyright
Public Use Permitted.
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