Volume 42 Issue 1
Feb.  2014
Turn off MathJax
Article Contents
Article Navigation >  Infrared and Laser Engineering  > 2013  >  42(1): 154-158

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.
shu

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

  • 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.
  • 加载中
通讯作者: 陈斌, bchen63@163.com
  • 1. 

    沈阳化工大学材料科学与工程学院 沈阳 110142

  1. 本站搜索
  2. 百度学术搜索
  3. 万方数据库搜索
  4. CNKI搜索
Get Citation
PDF
XML

Article Metrics

Article views(430) PDF downloads(142) Cited by()

Related
Proportional views

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
  • Received Date: 2012-05-22
  • Rev Recd Date: 2012-06-19
  • Publish Date: 2013-01-25

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.

    HTML

Reference (13)

Catalog

    版权所有 © 2019 《红外与激光工程》编辑部｜ Address: 58 Zhonghuan West Road, Tianjin Airport Economic Zone｜ Post Code: 300308

    津ICP备19007885号-1

    Supported by: Beijing Renhe Information Technology Co. Ltd  

    /

    DownLoad:  Full-Size Img  PowerPoint
    Return
    Return