|Table of Contents|

Recent development of radiation cooling body materials for liquid rocket engines(PDF)

《火箭推进》[ISSN:1672-9374/CN:CN 61-1436/V]

Issue:
2023年01期
Page:
12-20
Research Field:
目次
Publishing date:

Info

Title:
Recent development of radiation cooling body materials for liquid rocket engines
Author(s):
WANG Kai1;  ZHANG Peng1;  YANG Weipeng1;  ZHANG Weiming1;  LI Guangkuo2
(1.Xian Space Engine Company Limited, Xian 710100, China 2.Academy of Aerospace Propulsion Technology, Xian 710100, China)
Keywords:
radiant cooling body combustion chamber nozzle refractory metal composite material
PACS:
TG14 V45
DOI:
-
Abstract:
Radiation cooling is the most commonly used cooling method for the upper stage and space liquid rocket engine thrust chamber body, it has also been applied in several high thrust and high-performance second stage rocket engine nozzle recently.The high temperature resistance and density of radiation cooling body materials directly affect the specific impulse, thrust weight ratio and reliability of liquid rocket engine.By searching domestic and overseas literatures, researches and applications of titanium alloy, superalloy, refractory metal and C fiber composite in radiant cooling body of liquid rocket engines were reviewed.Combined with the working conditions of combustion chamber and nozzle of liquid rocket engines, the characteristics of different materials were analyzed.To study the development needs of high performance, high reliability and low cost liquid rocket engines in the future, an overview of the Ir/Re/C-C composites materials, low density niobium alloy and 3D printing refractory alloy that have gradually developed in recent years was carried out.

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