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X-38 De-Orbit Propulsion Stage MLI Performance TestThis viewgraph presentation gives an overview of the X-38 de-orbit propulsion stage MLI performance tests. The objectives of the research include the testing of the deorbit propulsion stage (DPS) multi-layer insulation (MLI) to determine if MLI performance meets or exceeds that assumed in thermal analysis and to determine the performance degradation due to seams.
Document ID
20020016969
Acquisition Source
Marshall Space Flight Center
Document Type
Preprint (Draft being sent to journal)
Authors
Kittredge, Ken (NASA Marshall Space Flight Center Huntsville, AL United States)
Hunt, Patrick L.
Date Acquired
September 7, 2013
Publication Date
January 1, 2001
Subject Category
Spacecraft Design, Testing And Performance
Meeting Information
Meeting: Thermal and Fluids Analysis Workshop
Location: Huntsville, AL
Country: United States
Start Date: September 10, 2001
End Date: September 14, 2001
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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