NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Back to Results
Heatshield material selection for advanced ballistic reentry vehiclesThe 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.
Document ID
19810005657
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Legendre, P. J.
(Aerospace Corp. El Segundo, CA, United States)
Holtz, T.
(Aerospace Corp. El Segundo, CA, United States)
Sikra, J. C.
(Air Force Ballistic Missile Office Norton AFB, Calif., United States)
Date Acquired
August 11, 2013
Publication Date
January 1, 1980
Publication Information
Publication: The 11th Space Simulation Conf.
Subject Category
Composite Materials
Accession Number
81N14169
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
No Preview Available