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Fabrication of prepackaged superalloy honeycomb Thermal Protection System (TPS) panelsHigh temperature materials were surveyed, and Inconel 617 and titanium were selected for application to a honeycomb TPS configuration designed to withstand 2000 F. The configuration was analyzed both thermally and structurally. Component and full-sized panels were fabricated and tested to obtain data for comparison with analysis. Results verified the panel design. Twenty five panels were delivered to NASA Langley Research Center for additional evaluation.
Document ID
19870020148
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Blair, W. (Rohr Industries, Inc. Chula Vista, CA, United States)
Meaney, J. E. (Rohr Industries, Inc. Chula Vista, CA, United States)
Rosenthal, H. A. (Rohr Industries, Inc. Chula Vista, CA, United States)
Date Acquired
September 5, 2013
Publication Date
October 1, 1985
Publication Information
Publisher: NASA
Subject Category
Launch Vehicles And Space Vehicles
Report/Patent Number
NASA-CR-3755
NAS 1.26:3755
Report Number: NASA-CR-3755
Report Number: NAS 1.26:3755
Accession Number
87N29581
Funding Number(s)
PROJECT: RTOP 506-53-33-07
CONTRACT_GRANT: NAS1-15646
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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