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Thermal and Structural Performance of Woven Carbon Cloth For Adaptive Deployable Entry and Placement Technology
Author(s) -
Keith Peterson,
Bryan Yount,
Nigel R. Schneider,
Dinesh Prabhu,
James O. Arnold,
Thomas H. Squire,
Paul Wercinski,
J. Chavez-Garcia,
Ethiraj Venkatapathy
Publication year - 2013
Publication title -
nasa sti repository (national aeronautics and space administration)
Language(s) - English
Resource type - Conference proceedings
DOI - 10.2514/6.2013-1370
Subject(s) - arcjet rocket , aerospace , thermal , materials science , aerospace engineering , carbon fibers , space shuttle thermal protection system , structural engineering , composite material , mechanical engineering , engineering , thermal protection , meteorology , physics , propellant , composite number
Arcjet 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.

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