实现高超声速跳跃式弹道关键问题的研究  

Study on Key Problems of Realizing Hypersonic Skip Trajectory

作　　者：马英[1] 何麟书[2] 

机构地区：[1]北京航空航天大学机械工程及自动化学院,北京100191 [2]北京航空航天大学宇航学院,北京100191

出　　处：《弹道学报》2009年第1期35-38,共4页Journal of Ballistics

摘　　要：为提高高超声速导弹的突防能力,使常规布局空中发射的高超声速巡航弹能采用跳跃式弹道突防,采用了在导弹再入段附加相应的正攻角产生气动升力的方法,找出了实现弹道起跳的关键参数,讨论了这些参数对弹道性能的影响.通过弹道仿真,针对初始质量为800 kg的空射导弹,实现了射程大于500 km,最大法向过载不超过10g,最大动压不超过1.5 MPa的跳跃式机动弹道.仿真结果表明,该文的飞行程序易于实现,只要关键参数在合理范围内,空射高超声速巡航弹就可在再入阶段实现跳跃机动.In order to improve penetrativity of hypersonic missile and enable air-launched hypersonic cruise missile to penetrate with skip trajectory, a new approach of generating positive angle of attack during reentry phase of trajectory was proposed. Some key parameters of realizing skip trajectory were found out, and the effects of these parameters on ballistic performance were discussed. Aiming at an 800 kg air-launched missile, skip trajectory with range of more than 500 km, normal overload of less than 10g and dynamic pressure of less than 1.5 MPa was realized by traiectory simulation. Simulation result indicates that the proposed flight program is easy to be realized, and skip trajectory of air-launched hypersonic missile can be realized if key parameters remain in reasonable range.

关 键 词：高超声速 跳跃弹道 弹道设计 飞行程序 

分 类 号：V412.1[航空宇航科学与技术—航空宇航推进理论与工程]