The Design and Analysis Program for the Development of LEO Satellite Electrical Power Subsystem

Astronomy and Astrophysics – Astronomy

Scientific paper

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Leo(Low Earth Orbit), Satellite, Eps(Electrical Power Subsystem), S/A(Solar Array), Battery, Ppt(Peak Power Tracking), Eb(Energy Balance)

Scientific paper

The design and analysis of satellite power subsystem is an important driver for the mass, size, and capability of the satellite. Every other satellite subsystem is affected by the power subsystem, and in particular, important issues such as launch vehicle selection, thermal design, and structural design are largely influenced by the capabilities and limitations of the power system. This paper introduces a new electrical power subsystem design program for the rapid development of LEO satellite and shows an example of design results using other LEO satellite design data. The results shows that the proposed design program can be used the optimum sizing and the analytical prediction of the on-orbit performance of satellite electrical power subsystem.

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