This site uses cookies. By continuing to use this site you agree to our use of cookies. To find out more, see our Privacy and Cookies policy.
Paper The following article is Open access

Ceramic Matrix Composite Materials for Structural Elements of Aviation and Rocket-Space Equipment

, and

Published under licence by IOP Publishing Ltd
, , Citation P A Stepanov et al 2020 IOP Conf. Ser.: Mater. Sci. Eng. 934 012058 DOI 10.1088/1757-899X/934/1/012058

1757-899X/934/1/012058

Abstract

Ceramic matrix composite materials based on inorganic binders (based on aluminum-chromium-phosphate binder and quartz glass slurry) and textured quartz filler are obtained by various molding methods at JSC ORPE Technologiya named after A.G. Romashin. The materials were studied in the high-temperature region (at the ambient temperature up to 1200°C during short-term exposure). The main specifications of the materials obtained in comparison with those of quartz ceramic material are shown.

Export citation and abstract BibTeX RIS

Content from this work may be used under the terms of the Creative Commons Attribution 3.0 licence. Any further distribution of this work must maintain attribution to the author(s) and the title of the work, journal citation and DOI.

Please wait… references are loading.
10.1088/1757-899X/934/1/012058