## Abstract Ceramic matrix composites (CMCs) based on zirconium diboride (ZrB~2~) reinforced by vapor grown carbon nanofibers are a potential constituent of reusable thermal protection systems. A manufacturing procedure was devised that involved the fabrication of thin films by tape casting to obta
β¦ LIBER β¦
Consolidation Process of PEEK/Carbon Composite for Aerospace Applications
β Scribed by J. Denault; M. Dumouchel
- Book ID
- 110264490
- Publisher
- Springer
- Year
- 1998
- Tongue
- English
- Weight
- 718 KB
- Volume
- 5
- Category
- Article
- ISSN
- 0929-1881
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