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The purpose of this paper is to have an optimized selection of solar cells for a telecommunication Nano-satellite by the maximum and the minimum longevity of 2 and 1 years, respectively. Also by considering the orbital height of 500 km, average power of 10.4 watt, maximum power of 35 watt, eclipse period of 35.75 minutes, and through the Direct Energy Transmission (DET) approach. At first, the subsystem’s required information of different telecommunication Nano-satellite will be collected, then the designing of satellite power system will be done based on a mathematical model. Then according to the simulation results in MATLAB/Simulink an optimized solar cell will be selected.

Optimized Selection of Solar Cell for A Nano-Satellite According to A Mathematical Model of Subsystem’s Required Power