摘要
阐述了脉冲爆震火箭发动机(PDRE)性能特点、结构和工作过程。采用航空煤油为燃料,氧气和压缩空气为氧化剂,分别进行了两相脉冲爆震火箭发动机原理性试验,所测得的爆震波压力接近充分发展的理想爆震波压力,说明采用煤油作为脉冲爆震火箭发动机的燃料是可行的。
The performance characteristics, structure and working cycle of pulse detonation rocket engine (PDRE) were introduced firstly.Then using kerosene as fuel, oxygen and compressed air as oxidizers,proof-of-principle experiments of PDRE were successfully conducted.The results show that the measured detonation wave pressures are close to theoretical values.It also indicate that using kerosene as the fuel of PDRE is feasible.
出处
《推进技术》
EI
CAS
CSCD
北大核心
2004年第5期450-453,共4页
Journal of Propulsion Technology
基金
国家自然科学基金(50106012
50336030)
教育部优秀青年教师资助计划
西北工业大学毕业设计重点扶持项目的资助。
