Study on Mechanical Properties of Carbon-Carbon Composites Developed for Aerospace Applications

被引：1

作者：

Simil, T. S. ^{[1
]}

Midhun, A. J. ^{[1
]}

James, V. J. ^{[1
]}

Lakshmidasan, S. K. ^{[1
]}

Usha, K. M. ^{[1
]}

Rakesh, S. ^{[1
]}

机构：

[1] ISRO, Vikram Sarabhai Space Ctr, Composites Ent, Trivandrum, Kerala, India

来源：

CARBON MATERIALS 2012 (CCM12): CARBON MATERIALS FOR ENERGY HARVESTING, ENVIRONMENT, NANOSCIENCE AND TECHNOLOGY | 2013年 / 1538卷

关键词：

Carbon-Carbon; Thermo-structural properties; Hot structures;

D O I：

10.1063/1.4810049

中图分类号：

TE [石油、天然气工业]; TK [能源与动力工程];

学科分类号：

0807 ; 0820 ;

摘要：

Carbon-carbon composites, which is a low density material exhibit remarkable thermo-structural properties. This makes it an ideal choice for realising products/hot structures for aerospace applications which encounters hostile thermal environments. As part of the carbon-carbon product development for spacecrafts and launch vehicles, VSSC-ISRO is in the development of carbon-carbon composites by means of distinct processing routes and fibre matrix combinations based on the application. Mechanical properties of the same were evaluated both in ambient as well as at elevated temperature regimes. Analysis of the test results reveals that the process combining graphitised carbon preform with densified matrix structure can lead to enhanced thermo-structural properties.

引用

页码：163 / 167

页数：5