摘要
介绍了含铝复合推进剂发动机试验时,对其喷管进行的烧蚀和温度场测量,获得了复合喷管结构中的烧蚀和瞬时温度分布.
The measurement of erosion and temperature field in the nozzle hat been made in the test of a solid motor loaded with the aluminized propellant. The data of erosion and temperature distribution in the composite nozzle structure have been obtained.
出处
《固体火箭技术》
EI
CAS
CSCD
1993年第3期31-36,共6页
Journal of Solid Rocket Technology
关键词
火箭发动机
喷管
烧蚀
温度分布
Subject Terms
Rocket motor nozzle
Erosion
Tempcrature distribution
Measurement
