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针对导弹武器对推力随机可控固体火箭发动机的需求,介绍了一种新型燃烧可控固体推进剂及其动力装置技术。具体介绍了燃烧可控固体推进剂的基本特征、各项性能、燃烧可控固体推进剂动力装置的连续性多次启动特性、推力主动实时可控特性及其应用进展。对燃烧可控固体推进剂动力装置技术的未来发展进行了展望,燃烧可控固体推进剂发动机有望取代液体姿轨控及末修发动机,作为导弹武器动力装置或辅助动力装置,可显著提升导弹武器生存能力及突防能力。
In view of the demand of missile weapon on the stochastic controllable solid propellant rocket engine, a new combustion controllable solid propellant and its power plant technology are introduced. In this paper, the basic characteristics of combustion controllable solid propellant, various properties, the characteristics of continuous multiple start-up, the active controllable real-time thrust characteristics and the application progress of the combustion controllable solid propellant power plant are introduced in detail. The future development of combustion controllable solid propellant power plant technology is prospected. Combustion controllable solid propellant engine is expected to replace liquid attitude and trajectory control and final engine repair. As a missile weapon power plant or auxiliary power plant, it can significantly enhance missile weapon Survivability and penetration ability.