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弹箭与制导学报 >

2011 , Vol. 31 >Issue 1: 135 - 136,230

DOI: https://doi.org/10.15892/j.cnki.djzdxb.2011.01.030

火箭技术

国外某型号发动机反设计

  • 邢国强 ,
  • 王君祺
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  • 中国空空导弹研究院,河南洛阳 471009

邢国强(1972-),男,河南伊川人,高级工程师,硕士,研究方向:空空导弹推进系统。

收稿日期: 2010-07-06

  网络出版日期: 2025-05-30

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The Analysis on Inverse Design of Solid Rocket Motor for Air-to-air Missile

  • XING Guoqiang ,
  • WANG Junqi
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  • China Airborne Missile Academy, Henan Luoyang 471009, China

Received date: 2010-07-06

  Online published: 2025-05-30

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摘要

对国外某型号发动机进行反设计,分析了该发动机的总体结构形式,依据测绘的药型和喷管几何参数,推算出推进剂的性能参数,并计算出内弹道曲线。改进型发动机和基本型相比,提高了性能,并且改善了装药可生产性。

关键词： 空空导弹; 固体火箭发动机; 反设计

本文引用格式

邢国强 , 王君祺 . 国外某型号发动机反设计[J]. 弹箭与制导学报, 2011 , 31(1) : 135 -136,230 . DOI: 10.15892/j.cnki.djzdxb.2011.01.030

Abstract

The inverse design analysis of solid rocket motor for air-to-air missile was conducted. The structure and pattern of the motor were analyzed. According to the geometry plotting parameter of the grain and the nozzle, the performance parameters of propellant were obtained, and interior ballistic curves were characterized. The improved motor for the air-to-air missile has better performance and production capacity of charge compared with basic motor.

Key words： air-to-air missile; solid propellant rocket motor; inverse design

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参考文献

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K M Crockett, M J Birch. The selection of the advanced medium range air-to-air rocket motor age-surveillance program, AIA A94-2916[R]. 1994.
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K M Crockett, M J Birch. The selection of the advanced medium range air-to-air rocket motor age-surveillance program; year 2. AIAA 95-2870[R]. 1995.
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http://www.atk.com[OL].
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谢文超, 徐东来, 蔡选义, 等. 空空导弹推进系统设计[M]. 北京: 国防工业出版社, 2006.
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