Search NASA⌕ Search

NASA NTRS · 19870000182

Ceramic Parts for Turbines

Abstract

Abilities of ceramics to serve as turbine blades, stator vanes, and other elements in hot-gas flow of rocket engines discussed in report. Ceramics prime candidates, because of resistance to heat, low density, and tolerance of hostile environments. Ceramics considered in report are silicon nitride, silicon carbide, and new generation of such ceramic composites as transformation-toughened zirconia and alumina and particulate- or whisker-reinforced matrices. Report predicts properly designed ceramic components viable in advanced high-temperature rocket engines and recommends future work.

Keep this discovery

Explore connections, maps & timelines

BibTeXRIS

Jones, R. D., Carpenter, Harry W., Tellier, Jim, Rollins, Clark, Stormo, Jerry. 1987-04-01. Ceramic Parts for Turbines. https://ntrs.nasa.gov/citations/19870000182

Cite the original work for its findings. Save a collection to share your selection of sources.