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NASA Shuttle Orbiter Reinforced Carbon Carbon (RCC) Crack Repair Arc-Jet TestingThis NASA study demonstrates the capability for testing NOAX-repaired RCC crack models in high temperature environments representative of Shuttle Orbiter during reentry. Analysis methods have provided correlation of test data with flight predictions. NOAX repair material for RCC is flown on every STS flight in the event such a repair is needed. Two final test reports are being generated on arc-jet results (both calibration model runs and repaired models runs).
Document ID
20070017880
Acquisition Source
Johnson Space Center
Document Type
Conference Paper
Authors
Clark, ShawnDella (Jacobs Sverdrup Technology, Inc. United States)
Larin, Max (Jacobs Sverdrup Technology, Inc. United States)
Rochelle, Bill (Jacobs Sverdrup Technology, Inc. United States)
Date Acquired
August 23, 2013
Publication Date
April 13, 2007
Subject Category
Composite Materials
Meeting Information
Meeting: ASME District E Student Professional Development
Location: Edinburg, TX
Country: United States
Start Date: April 12, 2007
End Date: April 14, 2007
Sponsors: American Society of Mechanical Engineers
Funding Number(s)
CONTRACT_GRANT: NNJ05HI05C
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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