| 摘要 |
<P>PROBLEM TO BE SOLVED: To provide a collecting device for solar energy for a space ship which can reduce a risk of a primary and a secondary electrostatic discharge. <P>SOLUTION: The present invention relates to a device which can reduce the risk of the primary and the secondary electrostatic discharge occurring particularly on a solar power generating device of a spaceship. The present invention relates to the collecting device of the solar energy for the space ship which is provided with at least one reflecting plate 12 for reflecting a solar radiation 16 to at least one photocell 14 for converting the solar energy to an electric energy. According to the present invention, this device is provided with heat transport means 23, 24 and 25 which can transport a thermal energy accumulated by the cell to a low-temperature zone 22 after receiving the sunlight. The present invention is applied particularly to a solar battery panel for a satellite. <P>COPYRIGHT: (C)2003,JPO |
