摘要
提出了催化燃烧双基推进剂在固体火箭发动机中可能出现几个平衡压力的看法。实验证实了此观点的正确性,并讨论了产生非唯一平衡压力的内在条件及外在原因。
A new concept that there could be more than one equivalent pressures in a solid rocket motor using double-base propellant has been put forward. This hypothesis has been confirmed by a few experiments. The authors have also discussed the conditions of existence of non-unique equivalent pressures.
出处
《推进技术》
EI
CAS
CSCD
北大核心
1993年第5期17-20,共4页
Journal of Propulsion Technology
关键词
固体推进剂
火箭发动机
燃烧
Solid propellant rocket engine, Solid Propellant, Combustion, Pressure, Aerodynamic balance