Statistical model of power supply subsystem Satellite

In this paper, based on the fact that in designing the energy providing subsystem for satellites, most approaches and relations are empirical and statistical, and also, considering the aerospace sciences and its relation with other engineering fields such as electrical engineering to be young, these are no analytic or one hundred percent proven empirical relations in many fields. Therefore, we consider the statistical design of this subsystem. The presented approach in this paper is entirely innovative and all parts of the energy providing subsystem for the satellite are specified. In codifying this approach, the data of 602 satellites and some software programs such as SPSS have been used. In this approach, after proposing the design procedure, the total needed power for the satellite, the mass of the energy providing subsystem, the material of solar array, and finally the placement of these arrays on the satellite are designed. All these parts are designed based on the mission of the satellite and its weight class.