[1] [1] ZHANG L, YAO J S, JIA X ZH, et al..Development of trusses made of carbon fiber composites for coaxial space remote sensors ［J］.Opt.Precision Eng., 2012, 20(9): 1967-1973.(in Chinese)

[2] [2] FAN B, WANG Y.Research on truss structure of foreign remote-sensing cameras with long focal length and high resolution ［J］.Spacecraft Recovey & Remote Sensing, 2008, 29(2): 35-41.(in Chinese)

[3] [3] ZHANG L, JIN G.Structure design and modes analysis for the truss of light high resolution space camera ［J］.Chin.J.Space Sci., 2008, 28(3): 260-263.(in Chinese)

[4] [4] ROBET C R.CFRP composites for optical and structures in telescope applications［C］.Proc.SPIE 2543, 1995, 2543: 154-161.

[5] [5] PAUL R Y, JR.Opto-Mechanical Systems Design［M］.Beijing: China Machine Press, 2008.

[6] [6] LIN W M, YUAN J L, BENGT S D.Review on graphite foam as thermal material for heat exchangers ［C］.World Renewable Energy Congress, 2011: 748-755.

[7] [7] ZHANG S H, MIKE V, PAUL B, et al..Evaluation and finite element modeling for new type of thermal material Annealed Pyrolytic Graphite (APG) ［J］.Thermochimicaacta, 2006, 6(9): 6-9.

[8] [8] LI J H, HAN SH L.Thermal analysis and thermal control techniques of space camera［J］.Opt.Precision Eng., 1999, 7(6): 36-41.(in Chinese)

[9] [9] Spacecraft thermal control［S］.NASA Space Vehicle Design Criteria, 1973.

[10] [10] PANCZAK T, WELCH M.Thermal Desktop User Manual, www.cretch.com［OL］..

[11] [11] Panasonic′s Thermally Conductive Pyrolytic Graphite Sheet (PGS).Panasonic Industrial Company Product Management Dept.2005［OL］.

[12] [12] EDWARD Silverman, MARK Montaesano.Development of an Annealed Pyrolytic Graphite Material for a Spacecraft Electronics Packaging Payload Module［OL］.NORTHOP GRUMMAN, 2004.

[13] [13] HOSEI N, AKIRA O.Development of a lightweight deployable/storable radiator for interplanetary exploration［J］.Applied Thermal Engineering, 2011(31): 3322-3331.

[14] [14] CULLIMORE B.Optimization, data correlation, and parametric analysis features in SINDA/Fluint version 4.0 ［J］.International Conference on Environmental Systems, 1998.

[15] [15] WU Q W, WANG L H, YANG X W et al..Application of carbon-carbon composites to thermal control of space optical instrument ［J］.Opt.Precision Eng., 2012, 20(9): 1984-1990.(inChinese)

[16] [16] DAVID G.Gilmore.Spacecraft Thermal Control Handbook-Volume I: Fundamental Technologies 2ndEd［M］.The Aerospace Press, El Segundo, CA, 90245-4691.

[17] [17] HOU Z Q, HU J G.Spacecraft Thermal Control-Fundamentals and Application［M］.Beijing: China Science & Technology Press, 2007.(in Chinese)