Abstract: Satellite solar generator wing including solar panels having at least two fixed solar panels and at least one semi-fixed solar panel. The solar panels are connected to one another in order to assume an operating position and a transport position, and, in the transport position, the solar panels are retained on top of one another and the semi-fixed solar panel is arranged in a freely oscillating manner between the two fixed solar panels.

Abstract: Satellite solar generator wing including solar panels having at least two fixed solar panels and at least one semi-fixed solar panel. The solar panels are connected to one another in order to assume an operating position and a transport position, and, in the transport position, the solar panels are retained on top of one another and the semi-fixed solar panel is arranged in a freely oscillating manner between the two fixed solar panels.

Abstract: A high electrical conductive, high temperature stable foil material, a process for the preparation of such a high electrical conductive, high temperature stable foil material, a solar cell interconnector including the high electrical conductive, high temperature stable foil material as well as the use of the high electrical conductive, high temperature stable foil material and/or the solar cell interconnector in solar power, aircraft or space applications. The high electrical conductive, high temperature stable foil material includes an aluminium alloy that has at least two elements selected from the group of scandium (Sc), magnesium (Mg), zirconium (Zr), ytterbium (Yb) and manganese (Mn).