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X-38 De-orbit Propulsion Stage MLI Performance TestThis paper presents a performance test of the X-38 Deorbit Propulsion Stage (DPS) Multi-Layer Insulation (MLI) system. The purpose of this test is to determine if MLI performance meets or exceeds thermal analyses requirements and if there is performance degradation due to seams.
Document ID
20030000768
Acquisition Source
Marshall Space Flight Center
Document Type
Conference Paper
Authors
Kittredge, Ken (NASA Marshall Space Flight Center Huntsville, AL United States)
Date Acquired
August 21, 2013
Publication Date
July 1, 2002
Publication Information
Publication: Twelfth Thermal and Fluids Analysis Workshop
Subject Category
Launch Vehicles And Launch Operations
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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IDRelationTitle20030000727Collected WorksTwelfth Thermal and Fluids Analysis Workshop
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