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亚燃或超燃冲压发动机推进的高性能导弹设计
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作者 丛敏 褚运 《飞航导弹》 2002年第10期5-10,共6页
叙述了远程高速飞行器弹体与推进系统一体化的设计方法。设计过程包括以下几个步骤 :1)制定性能准则 ;2 )改变发动机和弹体参数使性能最佳化 ;3)找出适合这些理想参数的布局。给出亚燃 /超燃冲压发动机性能的近似分析方法 ,并给出适当... 叙述了远程高速飞行器弹体与推进系统一体化的设计方法。设计过程包括以下几个步骤 :1)制定性能准则 ;2 )改变发动机和弹体参数使性能最佳化 ;3)找出适合这些理想参数的布局。给出亚燃 /超燃冲压发动机性能的近似分析方法 ,并给出适当的弹体参数。举例说明如何把这种方法应用到超燃冲压发动机推进的高超声速 (Ma =6 )导弹的初步设计中。 展开更多
关键词 超燃冲压发动机 高性能导弹 设计 亚燃冲压发动机 推进系统
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印度测试高性能反坦克导弹
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《国防科技》 2001年第9期87-87,共1页
关键词 印度 测试 高性能反坦克导弹 "毒蛇"
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X-35亚音速高性能反舰导弹
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《世界航空航天博览(B版)》 2004年第01B期10-10,共1页
X-35是前苏联/俄罗斯自行研制并装备部队使用的第四代反舰导弹,于1983年开始研制,1992年开始试飞,1993年投产,1995年进入海军舰队服役。装备水面舰艇直升机和飞机。
关键词 X-35型号 亚音速高性能反舰导弹 制导系统 抗干扰能力
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Three-time rapid transfer alignment method of SINS/GPS navigation system of high-speed marine missile 被引量:1
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作者 王司 邓正隆 苏凌峰 《Journal of Harbin Institute of Technology(New Series)》 EI CAS 2008年第2期244-247,共4页
The transfer alignment of SINS/GPS navigation system of a high-speed marine missile was investigated. With the help of the big acceleration of a high-speed missile, the transfer alignment was changed into a three-time... The transfer alignment of SINS/GPS navigation system of a high-speed marine missile was investigated. With the help of the big acceleration of a high-speed missile, the transfer alignment was changed into a three-time alignment. The azimuth alignment was coarsely finished in 10s in the first time alignment, the horizontal alignment was accurately and rapidly finished in the second time alignment, and the azimuth alignment was accurately finished in the third time alignment. Because the second time alignment and the third time alignment were finished by GPS after the missile was launched, the horizontal alignment and the second azimuth alignment got rid of the influence of the warship body flexibility deforming. The precision and rapidity of the horizontal alignment were prominently increased due to the vertical launch of the marine missile with the big acceleration. Simulation verifies the effectiveness of the proposed alignment method. 展开更多
关键词 inertial navigation SINS/GPS transfer alignment high-speed missile
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