MECHANICAL TESTING OF SILICA PHENOLIC COMPOSITES AT ELEVATED TEMPERATURES
Abstract
The principal objective of this study was to determine the mechanical properties, tensile yield, ultimate strength, and Young's modulus of elasticity of a silica fabric reinforced phenolic composite at temperatures above the cure level. The proposed application for this class of material as an ablative liner of a rocket nozzle skirt extension requires such engineering data for temperatures ranging up to 3000F so that design safety margins can be based on a thermostructural analysis.
Document Details
- Document Type
- Technical Report
- Publication Date
- Oct 01, 1968
- Accession Number
- AD0679981
Entities
People
- R. D. Carnahan
Organizations
- The Aerospace Corporation