[1] G DAVID. Spacecraft thermal control handbook volume i: fundamental technologies, 473-487(2002).

[2] S RIFFAT. Thermoelectrics: a review of present and potential applications. Applied Thermal Engineering, 23, 913-935(2003).

[3] NARASIMHA S, PATRICK J, SUDHIR B, et al. Nano engineering: fabrication, properties, optics, devices VⅡ[C]. SPIE, 2010, 7764: 776409.

[6] PEABODY H, STAVELY R, MAIDT D, et al. Development of a thermoelectric cooler simulation routine f the wide field camera 3 thermal model[C]. SAE, 2006012114.

[7] DU J, AU M, ZAVALA L, et al. Simple method f modeling thermoelectric cooler (TEC) perfmance of singleemitter semiconductlaser packages with concentrated heat sources[C]. SPIE, 2010, 7583: 75830l.

[8] D MARTIN. Spacecraft thermal control handbook volume Ⅱ: cryogenics, 1-12(2002).

[9] CHOI M. Thermal considerations of SWIFT XRT Radiat at 35℃ colder in low earth bit[C]. AIAA, 2000, 2906: 585594.

[10] CHOI M. AZWLAⅡ White paint on swift: lessons learned from first time flying on spacecraft radiats[C]. AIAA, 2004, 5685: 17.

[11] CHOI M. Maintaining swift XRT CCD temperature at 50℃ colder after TEC power supply failure[C]. AIAA, 2005, 5588: 111.

[12] BAGGET S, HILL R, KIMBLE R, et al. High energy, optical, infrared detects f astronomy Ⅲ[C]. SPIE, 2008, 7021: 70211Q.

[15] PEABODY H, STAVELY R, BAST W, et al. Lessons learned from the wide field camera 3 TV1 TV2 thermal vacuum test campaigns[C]. SAE, 2008012038.