摘要
对国内外冲压推进技术的发展现状进行了对比分析，论证了我国加快开展冲压发动机及相关技术研究的必要性。分析了冲压发动机驱动的导弹总体技术、进气道／转弯方式／冲压补燃室（无壅塞式应同时考虑燃气发生器）一体化设计、贫氧推进剂、燃气发生器、助推器及转级等方面的关键技术。
The development state of the ramjet and ducted rocketis in this field was reviewed. The key techniques in the development of solid ducted rocket, such as, the system design method, inlet/turn mode/ramcombustor uniform design techniques, fuel rich propellant, gas generator, air ducted combustion chamber, booster etc are analyzed
出处
《固体火箭技术》
EI
CAS
CSCD
1998年第3期24-30,共7页
Journal of Solid Rocket Technology
