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导弹与制导技术

燃气舵装置性能参数测试和分析

  • 王国锐 ,
  • 杜长宝
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  • 中国空空导弹研究院,河南洛阳 4710009

王国锐(1978-),男,河南洛阳人,工程师,研究方向:固体火箭发动机设计。

收稿日期: 2010-05-20

  网络出版日期: 2025-05-30

Test and Analysisof Jet Vane Device's Performance Parameter

  • WANG Guorui ,
  • DU Changbao
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  • China Airborne Missile Academy, Henan Luoyang 471009, China

Received date: 2010-05-20

  Online published: 2025-05-30

摘要

燃气舵装置性能参数的准确获得对导弹飞行控制性能设计非常重要。论述了燃气舵装置需要测试的性能参数、卧式六分力测试系统和燃气舵五分量天平测力系统的测试原理,介绍了两系统测试燃气舵性能参数的实现方法,分析了两系统影响测试精度的因素和优缺点,通过试验数据比较,指出了适合测试燃气舵各性能参数的试验方法。文中总结的测试和分析方法是合理、可行的。

本文引用格式

王国锐 , 杜长宝 . 燃气舵装置性能参数测试和分析[J]. 弹箭与制导学报, 2011 , 31(2) : 63 -64,156 . DOI: 10.15892/j.cnki.djzdxb.2011.02.055

Abstract

The accurate jet vane device's performance parameter is extremely important to the missile flying control performance design. The jet vane device's performance parameters needing test, and the principle of horizontal-type six-component test system and the jet vane five-component balance test system were presented, and the realization method testing jet vane performance parameter in two systems was analyzed, through the contrast result of testing data, the proper method that tests the jet vane performance parameters was pointed out. The testing and analysis methods summarized are reasonable and feasible.

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参考文献

[1]
Marti Sarigul-Klijn, Nesrin Sarigul-Klijn. Trade studies for air launching a small launch vehicle from a cargo aircraft, AIAA 2005-0621[R]. 2005.
[2]
何民. 内装式空射运载火箭初始弹道稳定方法研究[D]. 西安: 西北工业大学, 2010.
[3]
张登成, 闫杰, 张久星. 内装式空射运载火箭与载机分离研究[J]. 弹箭与制导学报, 2009, 29(5): 158-161.
[4]
王利荣. 降落伞理论与应用[M]. 北京: 宇航出版社, 1997.
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