[1] [1] MIN G R, GUO SH. Spacecraft Thermal Control[M]. Second Edition. Beijing: Science Press,1998. (in Chinese)

[2] [2] GOLDSTEIN R J, ECKERT E R G, IBELE W E, et al.. Heat transfer-a review of 2000 literature [J]. International Journal of Heat and Mass Transfer. 2002,45:2853-2957.

[3] [3] NG Y S, GORDON C A, JEFF A Y, et al.. Thermal modeling of the NASA-Ames research center cryogenic optical test facility and a single-arch, fused-natural-quartz mir-ror [J]. SPIE. 1990, 1340:122-133.

[4] [4] MARC D. RAFAL. Thermal design for the advanced camera for surveys [J]. SPIE.1998, 3356:301-307.

[5] [5] BADARI K, NARAYANA V. VENKATA R. Thermal design and performance of HAMSAT [J]. Acta Astronautica.2007, 60(1):7-16.

[6] [6] EDESON R L, SHAUGHNESSY B M, WHALLEY M S, et al.. The mechanical and thermal design and analysis of the VISTA infrared camera [J]. SPIE. 2004, 5947: 508-519.

[7] [7] ANESS A, THOMAS A, ROBERT G, et al.. Structural and thermal modeling of a cooled CCD camera [J]. SPIE. 2001, 4444:122-129.

[8] [8] CHEN SH P. Design and Test of Space Camera[M]. Beijing: Astronautic Publishing House, 2003. (in Chinese)

[9] [9] ZHANG SH J. Design and thermal analysis for depliyable space truss structure[D]. Hangzhou: Zhejiang University, 2005. (in Chinese)

[10] [10] CHEN L H, WU Q W, LUO ZH T, et al.. Design for thermal control system of electronic equipment in space camera [J].Opt. Precision Eng., 2009，17(9)：2145-2152. (in Chinese)

[11] [11] WANG J SH. Design of thermal equilibrium experiment device of space optical remote sensor [J]. Opt. Precision Eng., 2000, 8(6)：536-538. (in Chinese)

[12] [12] FAN H L, WEN Y P. Review on the thermal balance test for spacecraft[J]. Spacecraft Environment Engineering. 2007, 24(2): 63-68.(in Chinese)

[13] [13] LU E, YAN CH X, WU Q W, et al.. Research on adaptability of optical ranote sensors in mechanical and space thennal envirorments[J]. Chinese Journal of Optics and Applied Optics. 2009, 2(5): 364-376.(in Chinese)