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NASA NTRS · 19810005657

Heatshield material selection for advanced ballistic reentry vehicles

Abstract

The Performance of staple rayon fiber and AVTEX continuous rayon fiber was evaluated as precursor materials for heatshields. The materials studied were referenced to the IRC FM5055A heatshield materials flown during the past decade. Three different arc jet facilities were used to simulate portions of the reentry environment. The IRC FM5055A and the AVTEX FM5055G, both continuous rayon fiber woven materials having the phenolic impregnant filled with carbon particles were compared. The AVTEX continuous fiber, unfilled material FM5822A was also examined to a limited extent. Test results show that the AVTEX FM5055G material provided a close substitute for the IRC FM5055A material both in terms of thermal protection and roll torque performance.

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BibTeXRIS

Legendre, P. J., Holtz, T., Sikra, J. C.. 1980-01-01. Heatshield material selection for advanced ballistic reentry vehicles. https://ntrs.nasa.gov/citations/19810005657

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