摘要
本文根据发动机设计和试验中碰到的技术问题,简要论述固体火箭发动机喷管石墨喉衬温度场、应力场及其影响因素,提出在设计中值得注意的几个问题.
With technical problems met in development of motors,the temperature and the stress distributions in graphite throat liner of nozzle in solid rocket motors and the factors to effect them are brielly discussed in this paper.Several notables in design of nozzles are also proposed.
出处
《推进技术》
EI
CAS
CSCD
北大核心
1990年第5期35-38,共4页
Journal of Propulsion Technology
关键词
固体推进剂
火箭发动机
喷管
应力分析
Rocket engine nozzle, Nozzle throat, Stress analysis, Temperature distribution, Solid rocket engine, Design
