Thermal stability of CVI and MI SiC/SiC composites with Hi-Nicalon™-S fibers

Author:

Bhatt R.T.,Sola-Lopez F.,Halbig M.C.,Jaskowiak M.H.

Funder

National Aeronautics and Space Administration

Publisher

Elsevier BV

Subject

Materials Chemistry,Ceramics and Composites

Reference43 articles.

1. CMH-17 Composite Materials Handbook Volume 5, Ceramic Matrix Composites, Published by SAE International on behalf of CMH-17, a division of Wichita State University, June 2017.

2. Ceramic matrix composites taking flight at GE aviation;Steibel;Am. Ceram. Soc. Bull.,2019

3. C.M. Grondahl, and T. Tsuchiya, Performance benefit assessment of ceramic components in a MS9001FA gas turbine, Proceedings of ASME Turbo Expo 1998: Power for Land, Sea, and Air, ASME. 98-GT-186 (1998).

4. Ceramic-matrix composites;Donald;J. Mater. Sci.,1976

5. SiC/SiC composites for 1200°C and above;DiCarlo,2005

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