[1] Gilmore, D.G., Spacecraft Thermal Control Handbook, Vol. I: Fundamental Techniques, The Aerospace Corporation Press, 2002.
[2] Griffin, M.D. and French., J.R., Space Vehicle Design, Copyright© AIAA, Washington, DC, 1991.
[3] Martin, D., Parametric Models and Optimization for Rapid Thermal Design, MicroSat Systems Inc., Copyright© SAE International, 2004.
[4] Earth's Thermal Environment, Thermal Environments, JPL D-8160, K&K Associates, 2008.
[5] Orbit Definition, Structural Dynamics Research Corporation, 2001.
[6] Abouel-Fotouh, A.M, Elsharkawy, A.I., Shabaka, I. and Elfar, A., “The Effect of Satellite Orientation on Satellite Surface Temperature Distributions”, Journal of Applied Sciences Research, Vol. 2, No.12, 2006, pp.1286-1292.
[7] Method for the Calculation of Spacecraft Umbra and Penumbra Shadow Terminator Points, NASA Technical Paper 3547, 2002.
[8] Wertz, J.R. and Wiley J.L., Space Mission Analysis and Design, Microcosm Press, El Segundo CA, 1999, pp. 428-458.
[9] Eakman, D., Lambeck, R. and Slofer, L., Jr., Small Spacecraft Power and Thermal Subsystems, NASA Contractor Report 195029, Contract NASI-19244, Task 15, 1994.
[10]Silverman, E. M., Space Environmental Effects on Spacecraft: LEO Materials Selection Guide, NASA Contractor Report 4661, Parts 1 and 2, Prepared for Langley Research Center, 1995.
[11]Petrof, R.C. and Raynor S., “The Temperature Distribution in Rotating Thick-Walled Cylinders Heated by Radiation”, International Journal of Heat & Mass Trans., Vol. 11, Issue 3, 1968, pp. 427-438.
[12]Gadalla, M.A., “Analytical Modeling of Thermal Analysis of Rotating Space Vehicles Subjected to Solar Radiation”, Trans. Energy Conversion, American Chemical, 1993.
[13]Olmstead, W.E. and Raynor S., “Solar Heating of a Rotating Solid Cylinder”, Quarterly of Applied Mathematics, 1963, pp. 81-90.
[14]Nichols, L.D., Surface Temperature Distribution on Thin-walled Bodies Subjected to Solar Radiation in Interplanetary Space, NASA Technical Note D-584, USA, 1961.
[15]Gadalla, M. “Prediction of Temperature Variation in a Rotating Spacecraft in Space Environment,” Applied Thermal Engineering, Vol. 25, No. 14-15, 2005, pp. 2379-2397.
[16]Anvari, A., Farhani, F., Entezari, M.H. and Niaki, K.S., “Modeling and Thermal Analysis of Satellite Solar Panels”, The 8th Iranian Aerospace Society Conference (IAS2009), Malek-E-Ashtar University, Esfahan, Iran, 2009, (In Persian).
[17]Design of Hardware and Software for the Power Supply for AAU CubeSat, Appendix B, Group 02gr 733, 2002.
[18]Karam, R.D., Satellite Thermal Control for Systems Engineers, Vol. 181, Progress in Astronautics and Aeronautics, AIAA, Virginia, USA, 1998.
[19]Baturkin, V., “Micro-Satellite Thermal Control Concepts and Components”, ACTA Astronautica, Vol. 56, No.1-2, 2003, pp. 161-170.
[20] Galski, R.L., de Sousa, F.L., Ramos, F.M. and Muraoka, I., “Spacecraft Thermal Design with the Generalized External Optimization Algorithm,” Inverse Problems, Design and Optimization Symposium, Rio de Janeiro, Brazil, 2004.
[21]SINDA/FLUINT User’s Manual, Version 4.4, Cullimore and Ring Technologies Inc., 2001.
[22]Panczak T.D., Thermal Desktop, Version 4.4, Cullimore and Ring Technologies Inc., 2001.
[23]Badari and Venkata Reddy, “Thermal Design and Performance of HAMSAT,” Acta Astronautica, Vol. 60, Issue 1, 2007, pp. 7-16.