巡飞弹靶机动力及发射装置设计

Design of power and the launching device for loitering munition target drones

为提升巡飞弹靶机快速集群发射能力,扩大速度范围和续航能力,研究对燃油发动机改装修型、输出轴偏置、加装电起动组件和自动离合器技术,对火箭助推器和动力装置进行模块化协同设计,实现了燃油发动机在发射筒内自起动功能,发动机在火箭助推发射阶段保持连续性运转。使巡飞弹靶机具备了电动型/油动型巡飞弹作战模拟能力,提升了反巡飞弹对抗演练效能。

In order to improve the rapid cluster launching capability of the loitering munition target drone and expand the speed range and endurance capability,this paper researches on modification of fuel engine,output shaft offset,electric starting and automatic clutch,and carries out modular collaborative design of rocket boosters and power units.The self starting function of the fuel engine in the launcher is realized,and the engine maintains continuous operation during the rocket assisted launch phase.This enables the loitering munition target drones to have the capability of electric/oil powered missile patrol combat simulation,and improves the effectiveness of anti-loitering munition drills.