火箭发动机
液体火箭
火箭(武器)
推力
燃烧室
火箭发动机喷管
航空航天工程
燃烧室压力
冷却液
汽车工程
环境科学
工程类
材料科学
机械工程
燃烧
推进剂
化学
有机化学
冶金
作者
Yuanjie Qi,Yuqiang Cheng,Zhenzhen Zhang
标识
DOI:10.1109/isrimt53730.2021.9596851
摘要
Reusable rocket engine has become popular which is considered to decrease the cost of liquid rocket. Life always plays a crucial part in reusable rocket engine and it's necessary to predict the life of thrust chamber. Thrust chamber suffers from high temperature and pressure difference between gas-side wall and coolant channel which limits the life of rocket engine. In order to predict life of rocket engine, taking reusable liquid rocket engine as an investigated object and based on Porowski beam model. Porowski model calculates damage caused by fatigue, and thinning after each firing cycle. Damage results could predict life of reusable rocket engine which is manufactured by copper alloys. Life results are presented to evaluate which kind of material has better performance in reusable rocket engine.
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