Volume 34 Issue 3
May  2014
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Article Navigation >  Chinese Journal of Space Science  > 2014  >  34(3): 332-340
Dai Shuwu, Wu Ji, Sun Huixian, Zhang Baoming, Yang Jianfeng, Fang Guangyou, Wang Jianyu, Wang Huanyu, An Junshe. Chang’E-3 Lunar Rover’s Scientific Payloads[J]. Chinese Journal of Space Science, 2014, 34(3): 332-340. doi: 10.11728/cjss2014.03.332
Citation: Dai Shuwu, Wu Ji, Sun Huixian, Zhang Baoming, Yang Jianfeng, Fang Guangyou, Wang Jianyu, Wang Huanyu, An Junshe. Chang’E-3 Lunar Rover’s Scientific Payloads[J]. Chinese Journal of Space Science, 2014, 34(3): 332-340. doi: 10.11728/cjss2014.03.332
shu

Chang’E-3 Lunar Rover’s Scientific Payloads

doi: 10.11728/cjss2014.03.332 cstr: 32142.14.cjss2014.03.332
  • 1.

    Center for Space Science and Applied Research, Chinese Academy of Sciences, Beijing 100190

  • 2.

    Xi'an Institute of Optics and Precision Mechanics, Chinese Academy of Sciences, Xi'an 710068

  • 3.

    Institute of Electronics, Chinese Academy of Sciences, Beijing 100190

  • 4.

    Shanghai Institute of Technical Physics, Chinese Academy of Sciences, Shanghai 200083

  • 5.

    Institute of High Energy Physics, Chinese Academy of Sciences, Beijing 100049

  • Received Date: 2013-05-16
  • Rev Recd Date: 2014-01-04
  • Publish Date: 2014-05-15
    Abstract
  • Four scientific instruments are selected as the payloads for Chinese Chang'E-3 Lunar rover, including panoramic cameras, lunar radar, IR acousto-optic spectrometer, X-ray spectrometer. Panoramic cameras are to acquire the stereo optical image of lunar surface topography around the lunar rover. Lunar radar explores the lunar regolith thickness and structure. IR acousto-optic spectrometer obtains the IR spectrum and image of lunar surface, which can be used to analyze the lunar surface's mineral composition and distribution. X-ray spectrometer analyzes the content of the lunar surface rock to get the rock elements composition. In this paper, Chang'E-3 Lunar rover's scientific exploration objectives, the scientific payload's components and system design are mainly introduced. Each payload's design and main technical index are also described in detail.

     

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    • References(6)
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    Zhang Baoming. System design for CE-3 Lunar rover's payloads[R]. Beijing: Center for Space Science and Applied Research, Chinese Academy of Sciences, 2011. In Chinese (张宝明. CE-3巡视器有效载荷分系统设计报告, 北京: 中国科学院空间科学与应 用研究中心, 2011)
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    Korablev O, Bertaux J L, Fedorova A, et al. SPICAM IR acousto-optic spectrometer experiment on Mars Express. J. Geophys. Res., 2006, 111, doi: 10.1029/2006JE-002696-10.1029/2006JE002696
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    Wang Jie, Zeng Zuoxun, Yu Zongyu, et al. Research of lunar tectonic features: Primary results from Chang'E-1 lunar CCD image[J].Chin. J. Space Sci., 2011, 31(4): 482-491. In Chinese(王杰, 曾佐勋, 岳宗玉, 等. 月球主要构造特征: 嫦娥一号月球影像初步研究 [J]. 空间科学学报, 2011, 31(4): 482-491)
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