HSR/EPM combustor materials development program

Materials Science and Engineering: A

Volumn 261, Issue 1-2, 1999, Pages 284-291

  Brewer, David ^a  

^a NASA GLENN RESEARCH CENTER   (United States)

Author keywords

Combustor; SiC SiC ceramic matrix; Thermal conductivity

Indexed keywords

EID: 0039110377     PISSN: 09215093     EISSN: None     Source Type: Journal    
DOI: 10.1016/s0921-5093(98)01079-x     Document Type: Article

References (8)

1. Stephens, J., Herbell, T, Enabling Propulsion Materials for High-Speed Civil Transport Engines, NASA Langley Research Center, First Annual High-Speed Research Workshop, Part 3, April 1992 pp. 1523-1546.
2. DuPont Lanxide's New Material System for Long Life Performance in Oxidizing Environments, Newark, DE, Rev 1994.
3. DuPont CVI Ceramic Matrix Composites, Preliminary Engineering Data, DuPont Lanxide Composites, Newark, DE.
4. Besmann, T.M., Stinton, D.P., Lowden, R.A., Overview of chemical vapor infiltration, DE93-015440, Jan 1 1993.
5. Sylramic SiC Fiber Product Information Sheet, Dow Corning, Midland MI, 1997.
6. Worthem, D. Flat Tensile Specimen Design for Advanced Composites, NASA C.R. 185261, 1990.
7. Jacobson, N., Smialek, J. Fox, D. Opila, E. Durability of Silica Protected Ceramics in Combustion Atmospheres, NASA TM 112171, Jan 1995.
8. Robinson, R. SiC Recession Due to SiO2 Scale Volatility Under Combustor Conditions, NASA-CR-202331, May 1997.