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Thermal and Structural Performance of Woven Carbon Cloth For Adaptive Deployable Entry and Placement TechnologyArcjet testing and analysis of a three-dimensional (3D) woven carbon fabric has shown that it can be used as a thermal protection system and as a load bearing structural component for a low ballistic coefficient hypersonic decelerator called ADEPT (Adaptive Deployable Entry and Placement Technology). Results of arcjet tests proved that the 3D woven carbon fabric can withstand flight-like heating while under flight-like biaxial mechanical loads representative of those encountered during shallow entry flight path angles into the atmosphere of Venus. Importantly, the arcjet test results have been used to extend a preliminary material thermal response model based on previous testing of the same 3D woven carbon fabric under uni-axial mechanical loading.
Document ID
20140006949
Acquisition Source
Ames Research Center
Document Type
Conference Paper
Authors
Arnold, James O.
(NASA Ames Research Center Moffett Field, CA, United States)
Peterson, Keith H.
(Engineering Research and Consulting, Inc. Moffett Field, CA, United States)
Yount, Bryan C.
(NASA Ames Research Center Moffett Field, CA, United States)
Schneider, Nigel
(Northrop Grumman Corp. Hampton, VA, United States)
Chavez-Garcia, Jose
(Engineering Research and Consulting, Inc. Moffett Field, CA, United States)
Date Acquired
June 9, 2014
Publication Date
March 25, 2013
Subject Category
Aeronautics (General)
Report/Patent Number
ARC-E-DAA-TN8193
Meeting Information
Meeting: AIAA Aerodynamic Decelerator Systems Technology Conference
Location: Daytona Beach, FL
Country: United States
Start Date: March 25, 2013
End Date: March 28, 2013
Sponsors: American Inst. of Aeronautics and Astronautics
Funding Number(s)
CONTRACT_GRANT: NNL12AA09C
CONTRACT_GRANT: NNA10DE12C
Distribution Limits
Public
Copyright
Public Use Permitted.
Keywords
Carbon fabric
Woven TPS
ADEPT
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