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Analysis on the Mechanism of Fogging Inside the Photoelectric Seeker

  • FENG Tao 1 ,
  • SHI Mingdong 2 ,
  • ZHANG Peng 3 ,
  • DOU Yongpeng 3 ,
  • WU Hui 1 ,
  • LIANG Xiaobo 2 ,
  • QU Junli 2
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  • 1 Xi’an Modern Control Technology Research Institute,Xi’an 710065,Shaanxi,China
  • 2 Xi’an Guidance Technology Co.,Ltd.,Xi’an 710065,Shaanxi,China
  • 3 Xi’an Military Representative Bureau of Army Armament Department,Xi’an 710065,Shaanxi,China

Received date: 2024-01-31

  Online published: 2024-12-28

Abstract

The mechanism of low-temperature fogging in the photoelectric seeker of airborne missile is analyzed through theoretical analysis and experimental test. It is clarified that the respiration of the sealing structure during the temperature cycle is the main reason for the fogging phenomenon inside the seeker. The relationship between the water vapor content introduced by respiration and the structural leakage rate of the sealing structure under alternating temperature conditions is further deduced, which shows that the water vapor content introduced by respiration is exponentially positively correlated with the product leakage rate. The higher the leakage rate, the more water vapor is introduced by a single respiration. The higher the content, the easier it is to produce fogging phenomenon. exchange rate, and the easier the fog formation. When the leakage rate is lower than 1×10-6 Pa·m3/s, it can effectively reduce the gas exchange rate caused by respiration during the temperature cycle, and control the total gas exchange amount during temperature cycle screening within an acceptable range. Experimental verification was conducted on the number of temperature cycles required to produce fogging phenomenon under different leakage rates.

Cite this article

FENG Tao , SHI Mingdong , ZHANG Peng , DOU Yongpeng , WU Hui , LIANG Xiaobo , QU Junli . Analysis on the Mechanism of Fogging Inside the Photoelectric Seeker[J]. Journal of Projectiles, Rockets, Missiles and Guidance, 2024 , 44(1) : 84 -88 . DOI: 10.15892/j.cnki.djzdxb.2024.01.013

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[1]
肖军, 廖志忠, 吴连锋. 空空导弹弹体结构海洋环境腐蚀防护[J]. 航空兵器, 2019, 26(6): 86-92.

XIAO J, LIAO Z J, WU L F, et al. Study on corrosion protection on structure of air-to-air missiles in marine environment[J]. Aero Weaponry, 2019, 26(6): 86- 92.

[2]
肖军, 佘保民, 樊来恩, 等. 机载导弹包装箱技术及其研究进展[J]. 包装工程, 2010, 31(13): 136-139.

XIAO J, SHE B M, FAN L E, et al. Techniques of packaging case for airborne missiles and research developments[J]. Packaging Engineering, 2010, 31(13): 136-139.

[3]
朱觅, 王卫国, 吴昌. 某型空空导弹贮存寿命研究[J]. 国防技术基础, 2007(5): 40-44.

ZHU M, WANG W G, WU C. Research on storage life of a certain type of air to air missile[J]. Technology Foundation of National Defense, 2007(5): 40-44.

[4]
于运治, 李建林, 龚红良. 导弹贮存的失效模式及失效机理[J]. 四川兵工学报, 2009, 30(4): 27-29.

YU Y Z, LI J L, GONG H L. Failure modes and mechanisms of missile storage[J]. Journal of Sichuan Ordnance Engineering, 2009, 30(4): 27-29.

[5]
洪亮, 张福光, 崔旭涛. 海军导弹服役环境对导弹寿命的影响及防护包装对策的研究[J]. 包装工程, 2011, 32(23): 1-4.

HONG L, ZHANG F G, CUI X T. Research on influence of navai missile service environment on missile life and countermeasures of protection packaging[J]. Packaging Engineering, 2011, 32(23): 1-4.

[6]
赵建忠, 叶文, 田建海. 舰载环境对导弹武器装备可靠性的影响分析及对策[J]. 质量与可靠性, 2014(2): 5-9.

ZHAO J Z, YE W, TIAN J H. Analysis and countermeasures of the impact of shipborne environment on the reliability of missile weapon equipment[J]. Quality and Reliability, 2014(2): 5-9.

[7]
蔡培培, 胡凯征, 胡晓辉. 空空导弹弹体结构三防设计浅析[J]. 航空制造技术, 2012(19): 73-75.

CAI P P, HU K Z, HU X H. Research on three-prevention design of airborne missile body structure[J]. Aeronautical Manufacturing Technology, 2012(19): 73-75.

[8]
刘志, 罗吉, 任国华, 等. 温度循环条件下某光电舱结雾现象分析[J]. 航天器环境工程, 2017: 38-43.

LIU Z, LUO J, REN G H, et al. Analysis of fogging phenomenon in a sealed cabin under condition of temperature cycling[J]. Spacecraft Environment Engineering, 2017: 38-43.

[9]
陈松林, 王奎占, 沈颖. 某型空空导弹进水原因和对策[J]. 航空兵器, 2003(5): 18-19.

CHEN S L, WANG K Z, SHEN Y. Reasons and countermeasures for water ingress into a certain type of air-to-air missile[J]. Aero Weaponry, 2003(5): 18-19.

[10]
梁子豪, 刘仙名, 黄帅军. 空空导弹典型部位密封优化设计与试验验证[J]. 液压气动与密封, 2019, 39(11): 42-46.

LIANG Z H, LIU X M, HUANG S J. Seal optimization and test verification of air-to-air missile typical parts[J]. Hydraulics Pneumatics and Seals, 2019, 39(11): 42-46.

[11]
洪津, 孙彦青, 袁建虎, 等. 工程装备光学仪器的防霉防雾研究[J]. 机械工程与自动化, 2012: 191-193.

HONG J, SUN Y Q, YUAN J H, et al. Study on antimildew and antifog of optical instruments for engineering equipment[J]. Mechanical Engineering and Automation, 2012: 191-193.

[12]
王凡, 陈光奇, 王荣总. 航天产品常用泄漏检测方法[J]. 真空与低温, 2012, 18(12): 235-240.

WANG F, CHEN G Q, WANG R Z. Leak test method analysis of spacecraft[J]. Vacuum and Cryogenics, 2012, 18(12): 235-240.

[13]
刘燚, 刘贝贝, 周宇仁, 等. 基于不同气体和压力下通道型正压标准漏孔泄漏率的分析[J]. 上海计量测试, 2022, 49(1): 31-33.

LIU Y, LIU B B, ZHOU Y R, et al. Analysis of leakage rate of channel positive pressure standard leakage hole based on different gas and pressure[J]. Shanghai Measurement and Testing, 2022, 49(1): 31-33.

[14]
刘赐贤, 张涤新, 冯焱, 等. 金属压扁型正压漏孔不同压力下的泄漏率研究[J]. 真空与低温, 2011, 17(4): 218-223.

LIU C X, ZHANG D X, FENG, Y, et al. Research on leakage rate of metal flattening pressure leak with different pressures[J]. Vacuum and Cryogenics, 2011, 17(4): 218-223.

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