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Arcjet Testing and Thermal Model Development for Multilayer Felt Reusable Surface InsulationFelt Reusable Surface Insulation was used extensively on leeward external surfaces of the Shuttle Orbiter, where the material is reusable for temperatures up to 670 K. For application on leeward surfaces of the Orion Multi-Purpose Crew Vehicle, where predicted temperatures reach 1620 K, the material functions as a pyrolyzing conformal ablator. An arcjet test series was conducted to assess the performance of multilayer Felt Reusable Surface Insulation at high temperatures, and a thermal-response, pyrolysis, and ablation model was developed. Model predictions compare favorably with the arcjet test data
Document ID
20120016059
Acquisition Source
Ames Research Center
Document Type
Conference Paper
Authors
Milos, Frank S.
(NASA Ames Research Center Moffett Field, CA, United States)
Scott, Carl Douglas
(Jacobs Technology, Inc. Moffett Field, CA, United States)
Papa, Steven V.
(NASA Ames Research Center Moffett Field, CA, United States)
Date Acquired
August 26, 2013
Publication Date
June 25, 2012
Subject Category
Composite Materials
Report/Patent Number
ARC-E-DAA-TN5336
ARC-E-DAA-TN440
TSM-5336
Report Number: ARC-E-DAA-TN5336
Report Number: ARC-E-DAA-TN440
Report Number: TSM-5336
Meeting Information
Meeting: 43rd AIAA Thermophysics Conference
Location: New Orleans, LA
Country: United States
Start Date: June 25, 2012
End Date: June 28, 2012
Sponsors: American Inst. of Aeronautics and Astronautics
Funding Number(s)
CONTRACT_GRANT: NNJ05HI05C
Distribution Limits
Public
Copyright
Public Use Permitted.
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