Paper Title
Simplified Thermal Analysis of a CubeSat for Different Panel Combinations

Abstract
Manage the temperature of nanosatellite is the main challenge of thermal engineer, the payload, and the platform should kept within their acceptable marge of temperature during the mission. A simplified thermal model was designed and examined in order to determine the temperature of the Cube Sat. The paper presents a result of simulation of a 3U Cube Sat in orbit 600Km for a various combination for panels for a best compromise between the thermal control and the allowable power. Keywords - Thermal Analysis, Cube Sat, Panel, Thermal Control.