Calibration of 3D Woven Preform Design Code for CMC Materials

Period of Performance: 01/01/2009 - 12/31/2009

$100K

Phase 1 SBIR

Recipient Firm

Materials Research & Design
300 E. Swedesford Rd Array
Wayne, PA 19087
Principal Investigator

Abstract

Future hypersonic vehicles will utilize thermal protection system (TPS) designs and propulsion system components that are capable of experiencing high temperatures within oxidative environments during their operation. These TPS and propulsion system components will include high temperature ceramic matrix composites (CMCs), such as C/SiC and SiC/SiC. Both hot structure control surfaces and hot wall propulsion system components are two examples of CMCs for which prototype parts have thus far been fabricated and subjected to mechanical performance and/or durability testing.