Introduction
Among the different solar space power systems to be used on Mars a leading position is played by the photovoltaic (shortly, PV) solar cells. Due to their relatively low cost power, high reliability and the lack of moving parts they powered the space program from the very beginning (Landis and Appelbaum 1991). As a result the array manufacturing technology is now well developed, and the technology is well characterized for vibration, thermal-cycling, and other environmental loads of the space environment. A number of studies concerning the usage of PV cells on the Mars surface have been performed during the years and we quote here some of them. A rover powered by a PV array was designed in Hibbs (1989). To add robustness, a fixed array rather than one which tracks the sun was envisaged, because of the modest power requirements (275 Watt average power and peak power capability of up to 2000 W during climbing over large boulders). The array surface was as large as 7 m2. Another study refers to a long-endurance, remotely piloted aircraft capable of flight within the Martian environment (Colozza 1990). There is a variety of mission scenarios which would be possible with this aircraft ranging from magnetic and gravity field mapping to surveillance / reconnaissance missions. The flight duration would be on the order of one year. The power and propulsion systems consist of solar PV array panels, a regenerative fuel cell and an electric motor. Depending on the solar cell type the required PV array surface could be quite large (from 336 to 405 m2 in case of silicon-based solar cells or from 118 to 166 m2 when gallium arsenide PV arrays are used). A solar power system for a 40 day manned Mars surface scientific expedition was studied in McKissock et al. (1990). The electrical power requirements were assumed to be 40 kW for life support and experiment power during the Martian day and 20 kW for life support during the Martian night. The solar energy system consisted of roll out amorphous silicon arrays and a hydrogen - oxygen regenerative fuel cell energy storage system. The total array covers 2822 m2 when deployed and has a blanket mass of 177.6 kg.
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Badescu, V. (2009). Weather Influence on PV Solar Cells Operation on Mars. In: Badescu, V. (eds) Mars. Springer, Berlin, Heidelberg. https://doi.org/10.1007/978-3-642-03629-3_3
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