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Overview of CEV Thermal Protection System Seal DevelopmentNASA GRC supporting design, development, and implementation of numerous seal systems for the Orion CEV: a) HS-to-BS interface. b) Compression pad. HS-to-BS Interface Seal System: a) design has evolved as a result of changes with the CEV TPS. b) Seal system is currently under development/evaluation. Coupon level tests, Arc jet tests, and Validation test development. Compression Pad: a) Finalizing design options. b) Evaluating material candidates.
Document ID
20090041727
Acquisition Source
Glenn Research Center
Document Type
Conference Paper
Authors
DeMange, Jeff (Toledo Univ. Toledo, OH, United States)
Taylor, Shawn (Toledo Univ. Toledo, OH, United States)
Dunlap, Patrick (NASA Glenn Research Center Cleveland, OH, United States)
Steinetz, Bruce (NASA Glenn Research Center Cleveland, OH, United States)
Delgado, Irebert (NASA Glenn Research Center Cleveland, OH, United States)
Finkbeiner, Josh (NASA Glenn Research Center Cleveland, OH, United States)
Mayer, John (Analex Corp. Cleveland, OH, United States)
Date Acquired
August 24, 2013
Publication Date
November 1, 2009
Publication Information
Publication: 2008 NASA Seal/Secondary Air System Workshop
Subject Category
Mechanical Engineering
Distribution Limits
Public
Copyright
Public Use Permitted.

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