| 提高红外空对空导弹动力射程的技术途径 |
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| 引用本文： | 马文政.提高红外空对空导弹动力射程的技术途径[J].战术导弹技术,1992(3):7-9,46. |
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| 作者姓名： | 马文政 |
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| 作者单位： | 航空航天部014中心 |
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| 摘 要： | 根据对现有国内外红外空对空导弹的性能数据进行统计,总结出估算红外空对空导弹动力射程的经验公式.该公式用于导弹初步设计和评价国内外空对空导弹的性能是行之有效的.指出采用推力矢量控制技术是提高红外空对空导弹性能的重要技术途径.
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| 关 键 词： | 空对空 导弹 红外 制导 射程 |
TECHNICAL APPROACH TO IMPROVE THE MAXIMUM POWERED RANGE OF IR AIR TO AIR MISSILE |
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| Ma Wenzheng Electro-optical Technology Development Centre of MAS.TECHNICAL APPROACH TO IMPROVE THE MAXIMUM POWERED RANGE OF IR AIR TO AIR MISSILE[J].Tactical Missile Technology,1992(3):7-9,46. |
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| Authors: | Ma Wenzheng Electro-optical Technology Development Centre of MAS |
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| Affiliation: | Ma Wenzheng Electro-optical Technology Development Centre of MAS |
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| Abstract: | An empirical formula for estimation of the maximum powered range of IR air to air missile is given. Derived fiom the specifications of present IR air to air missiles at home and abroad, the formula is useful for concept design and evaluation of the performance of the missile. It is also shown that the thrust vector control is an important techmical approach to improve the performance of IR air to air missile. |
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| Keywords: | Air to air missile Irtfrarcd guidance Range |
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