Optics and Precision Engineering, Volume. 17, Issue 11, 2665(2009)
Thermal design of CCD focal plane assemblies for attitude-varied space cameras
[1] [1] ZI K M, WU Q W, GUO J, et al.. Thermal design of CCD focal plane assembly of space optical remote-sensor[J].Optical Technique,2008,3(34):401-403. (in Chinese)
[2] [2] CHEN E T, LU E. Thermal engineering design of CCD component of space remote-sensor[J]. Opt. Precision Eng., 2000, 8(6): 522-525. (in Chinese)
[4] [4] CAO D J, XIANG W G. Thermal control system of CBERS-1 satellite CCD camera[J]. Spacecraft Recovery &Remote Sensing, 2003,24(1):24-28. (in Chinese)
[5] [5] LI G Q, JIA H. Thermal analysis and thermal balance test of CCD assembly[J]. Spacecraft Recovery &Remote Sensing, 2003,24(3):15-18. (in Chinese)
[6] [6] DAVID B, MATTHEW B, CHARLES S, et al.. Advanced cryogenic thermal switches for JWST[J].SPIE, 2005, 5904:59040F1-F7.
[7] [7] MIN G R, GUO SH. Spacecraft Thermal Control[M]. Beijing: Science Press, 1998. (in Chinese)
[9] [9] LU E, NIU X M. Study on thermal control design of space camera based on CAD/CAE/CAT [J].Opt. Precision Eng.,1998,6(6):21-32.(in Chinese)
Get Citation
Copy Citation Text
HAN Dong, WU Qing-wen, LU E, CHEN Li-heng, YANG Cheng-yu. Thermal design of CCD focal plane assemblies for attitude-varied space cameras[J]. Optics and Precision Engineering, 2009, 17(11): 2665
Received: Oct. 22, 2008
Accepted: --
Published Online: Aug. 31, 2010
The Author Email: Dong HAN (leaf_hd@163.com)
CSTR:32186.14.