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- W2912256852 abstract "The power source is a crucial parameter in the field of micro-satellites. This paper aims to investigate the effect of using the solar power source of different technologies and configurations on the economic side including the economic income return of the satellite from increasing the payloads or by reducing the thrust required for launching or whether by increasing its lifetime. Considering a typical LEO micro-satellite, this paper illustrates the main design of solar and battery EPS with different orbits parameters such as its period, duration of eclipse and incident solar irradiance for different types of solar cells. Furthermore, the integration of solar power in the electric propulsion, rather than the usage of fuel, is shown with concluding its positive impacts on the economic side by reducing the satellite's weight and hence the launching cost and increasing its lifetime. Finally, a brief discussion on the usage of deployed wings for solar modules that can increase its lifetime without affecting its standard volume. The conclusion is summarized to show all different results of this paper's research and development." @default.
- W2912256852 created "2019-02-21" @default.
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- W2912256852 date "2018-12-01" @default.
- W2912256852 modified "2023-09-23" @default.
- W2912256852 title "Design PV for a CubeSat and Effect of the Electric Propulsion and Deployed Wings in the Lifetime" @default.
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- W2912256852 doi "https://doi.org/10.1109/mepcon.2018.8635169" @default.
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