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NASA NTRS · 20040020118

High Temperature Polymeric Materials for Space Transportation Propulsion Applications

Abstract

High temperature polymer matrix composites are attractive materials for space transporation propulsion systems because of their low density and high specific strength. However, the relatively poor stability and processability of these materials can render them unsuitable for many of these applications. New polymeric materials have been developed under the Propulsion Research and Technology Program through the use of novel resin chemistry and nanotechnology. These new materials can significantly enhance the durability and weight and improve the processability and affordability of propulsion components for advanced space transportation systems.

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BibTeXRIS

Meador, Michael A., Campbell, Sandi G., Chuang, Kathy C., Scheimann, Daniel A., Mintz, Eric, Hylton, Donald, Veazie, David, Criss, James, Kollmansberg, Ron, Tsotsis, Tom. 2003-01-01. High Temperature Polymeric Materials for Space Transportation Propulsion Applications. https://ntrs.nasa.gov/citations/20040020118

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