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C/sic life prediction for propulsion applications
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Verrilli, Michael J. Halbig, Michael C. Thomas, David J. Calomino, Anthony M. Opila, Elizabeth J. Levine, Stanley R. |
| Copyright Year | 2003 |
| Description | Accurate life prediction is critical to successful use of ceramic matrix composites (CMCs). 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 reusable and single mission launch vehicle propulsion and airframe 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 of C/SiC. |
| File Size | 11175008 |
| Page Count | 23 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_20040111984 |
| Archival Resource Key | ark:/13960/t26b23f9t |
| Language | English |
| Publisher Date | 2003-08-29 |
| Access Restriction | Open |
| Subject Keyword | Composite Materials Ceramic Matrix Composites Airframes Life Durability Performance Prediction Mechanical Properties Silicon Carbides Creep Rupture Strength Oxidation Water Vapor Reusable Launch Vehicles Ntrs Nasa Technical Reports Server (ntrs) Nasa Technical Reports Server Aerodynamics Aircraft Aerospace Engineering Aerospace Aeronautic Space Science |
| Content Type | Text |
| Resource Type | Article |
