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机载反舰导弹飞行方案研究
RESEARCH FOR FLIGHT PLANNING OF AIRBORNE AIR TO SHIP MISSIIE
【摘要】 研究了近程空舰导弹两种飞行方案的设计及弹道计算方法,并以某型导弹为例进行了计算。其结果可为机载反舰导弹总体设计提供参考。
【Abstract】 Two flight plannings and trajectory calculation method of short-range air-to-ship missile are studied. Calculation for certain missile as an example is made. The result obainted can be used for preliminary design of airborne air-to-ship missile as reference.
- 【文献出处】 战术导弹技术 ,Tactical Missile Technology , 编辑部邮箱 ,1995年02期
- 【分类号】TJ761.14
- 【下载频次】62