| 摘要 |
PROBLEM TO BE SOLVED: To firmly assemble a solar panel assembly for a space craft, to considerably reduce the cost, and to achieve the remarkable efficiency. SOLUTION: This solar cell assembly 50 is a rectangular flat solar cell 52 having four corner positions 54, 60; 56, 58, one of the corner positions has a diagonal edge 54, first conductive means 68, 70, 74 and second conductive means (for example, a metal coating) are provided on first and second surfaces opposite to each other of the flat solar cell, a bypass diode 84 which is a current limit protective function of the solar cell is carried by an interconnect means in the vicinity of the diagonal edge, the interconnect means absorbs the motion in the relative plane direction between the bypass diode and the solar cell by the stress buffer function, and the bypass diode is arranged electrically in the middle of the first and second conductive means, and connected thereto in series. |
