Long-term firing tests of the nozzles of rocket engines made on the basis of carbon composite materials

被引：0
|
作者：
A. M. Gubertov
V. V. Koshlakov
V. V. Mironov
V. R. Rubinskii
A. V. Pashutov
Ye. A. Antipov
N. A. Bratukhin
N. N. Volkov
L. I. Volkova
S. M. Tsatsuev
V. V. Tlevtsezhev
机构：
[1] Federal State Unitary Enterprise “Keldysh Research Center,State Scientific Center
[2] ”,undefined
[3] JSC Chemical Automation Design Bureau,undefined
[4] JSC Central Research Institute for Special Machinery,undefined
来源：
Thermal Engineering | 2012年 / 59卷 / 14期
关键词：
Combustion Chamber; Combustion Product; Propulsion System; Infrared Imager; Firing Test;
D O I：
10.1134/S0040601512140042
中图分类号：
学科分类号：
摘要：
The results of the experimental investigation of the physico-chemical processes of interaction, destruction, and ablation of carbon composite materials and oxidation-protective coatings of nozzles of liquid-propellant rocket engines are presented. The thermally-stressed state of the joint between the nozzle made of composite material and the metallic combustion chamber of the rocket engine under standard operating conditions have been analyzed.
引用
收藏
页码：1068 / 1073
页数：5
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