Volume 42 Issue 1
Feb.  2014
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Zhang Ke, Chen Zhiguang, Zhao Yuyin. Dome protecting technologies for overseas high-velocity guided missiles[J]. Infrared and Laser Engineering, 2013, 42(1): 154-158.
Citation: Zhang Ke, Chen Zhiguang, Zhao Yuyin. Dome protecting technologies for overseas high-velocity guided missiles[J]. Infrared and Laser Engineering, 2013, 42(1): 154-158.

Dome protecting technologies for overseas high-velocity guided missiles

  • Received Date: 2012-05-22
  • Rev Recd Date: 2012-06-19
  • Publish Date: 2013-01-25
  • A summary of dome protecting technologies design of high-velocity guided missiles was made in this paper. Based on a lot of US patents and other references, the classification of dome protecting design methods and analysis of the strengths and weaknesses and the scope of application of the various technologies was made. The temperature and thermal stress of the dome surface increased as the rise of the missile flight. Mach 2.5 is usually considered to be the thermal barrier boundary in aviation world. Conventional methods and materials can be used to design and manufacture aircraft when temperature is below this boundary, otherwise some measures must be taken to overcome the problem of aerodynamic heating, such as removal of a dome cover, installation of the shock wave cone, dome outline design and dome cooling technology.
  • [1]
    [2] Rockwell International Corporation (Seal Beach, CA). Removable radome cover: US, 5125600[P]. 1991-06-03.
    [3] Rockwell International Corporation (Seal Beach, CA). Pyrotechnic removal of a radome cover: US, 5167386[P]. 1992-01-21.
    [4]
    [5] The United States of America as represented by the Secretary of the Air. Protective cover for a missile nose cone: US, 3970006[P]. 1975-01-16
    [6]
    [7]
    [8] General Dynamics Corp, Pomona Division (Pomona, CA). Jettisonable protective cover device: US, 4867357[P]. 1987-12-21.
    [9]
    [10] The United States of America as represented by the Secretary of the Air (Washington, DC). Optical dome protection device: 4275859[P]. 1979-12-18
    [11] Raytheon Company (Lexington, MA) . Internal fluid cooled window assembly: 6530539[P]. 2001-02-09.
    [12]
    [13] Bodenseewerk Geratetechnik GmbH (Uberlingen/Bodensee, DE). Seeker head assembly in a guided missile: US, 5372333[P]. 1992-04-10.
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Dome protecting technologies for overseas high-velocity guided missiles

  • 1. School of Astronautics,Northwestern Polytechnical University,Xi'an 710072,China;
  • 2. Beijing Institute of Remote Sensing Equipment,Beijing 100854,China

Abstract: A summary of dome protecting technologies design of high-velocity guided missiles was made in this paper. Based on a lot of US patents and other references, the classification of dome protecting design methods and analysis of the strengths and weaknesses and the scope of application of the various technologies was made. The temperature and thermal stress of the dome surface increased as the rise of the missile flight. Mach 2.5 is usually considered to be the thermal barrier boundary in aviation world. Conventional methods and materials can be used to design and manufacture aircraft when temperature is below this boundary, otherwise some measures must be taken to overcome the problem of aerodynamic heating, such as removal of a dome cover, installation of the shock wave cone, dome outline design and dome cooling technology.

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