摘要
用压力可控Ｔ形燃烧器测量了三种无烟推进剂压力耦合响应函数，总结到一些实验规律，提出燃烧催化剂对抑制不稳定燃烧可能起到的重要作用。
Using pressure-controlled T-burner the anthors have determined the pressure coupling responses of three smokeless solid propellants. From the experiment results we have believed that the combustion catalyst may play an important role in eliminating the combustion instability in a solid rocket motor.
出处
《推进技术》
EI
CAS
CSCD
北大核心
1994年第5期62-66,共5页
Journal of Propulsion Technology
关键词
固体推进剂
火箭发动机
无烟推进剂
双基推进剂
Solid propellant rocket engine
Smokeless propellant
Double base propellant
Burner
Combustion stability
Pressure oscillation
Catalyst
