NASA NTRS · 20050214476
Ceramic Matrix Composites (CMC) Life Prediction Development
Abstract
Advanced launch systems will very likely incorporate fiber reinforced ceramic matrix composites (CMC) in critical propulsion and airframe components. The use of CMC will save weight, increase operating margin, safety and performance, and improve reuse capability. For reusable and single mission use, accurate life prediction is critical to success. The tools to accomplish this are immature and not oriented toward the behavior of carbon fiber reinforced silicon carbide (C/SiC), the primary system of interest for many applications. This paper describes an approach and progress made to satisfy the need to develop an integrated life prediction system that addresses mechanical durability and environmental degradation.
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Levine, Stanley R., Verrilli, Michael J., Thomas, David J., Halbig, Michael C., Calomino, Anthony M., Ellis, John R., Opila, Elizabeth J.. 1990-01-15. Ceramic Matrix Composites (CMC) Life Prediction Development. https://ntrs.nasa.gov/citations/20050214476
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