Affiliation:
1. Snecma Propulsion Solide
Abstract
Since more than twenty five years, composite materials have been with continuously
increasing spatial and aeronautical applications requirements. The thermostructural composites
materials are of utmost importance for satisfying the needs of mechanical and thermal characteristics
at very high temperature and in severe environments. This paper deals with a large variety of
applications concerning the aerospace and nuclear applications like nozzles and hot gas valves for
Solid Rocket Motor (SRM), brake disks for planes, aerospace turbine engine exhaust nozzles,
thermal protection system for reentry vehicles, but also Divert and Attitude Control System (DACS)
for interceptors, heat exchangers for hypersonic propulsion systems, plasma facing components for
nuclear fusion applications and special components for nuclear fission applications. We will see that
Carbon/Carbon and Ceramic Matrix Composites are leading candidate materials for these hightemperature
structural applications. This lecture will identify the current state-of-the-art and new
technological developments. A description of the main steps of the manufacturing processes will be
made.
Publisher
Trans Tech Publications Ltd
Cited by
29 articles.
订阅此论文施引文献
订阅此论文施引文献,注册后可以免费订阅5篇论文的施引文献,订阅后可以查看论文全部施引文献