(DE19728844-A1)      The system includes solar panels (3-7) on a space satellite (1) supported on an out rigger that is fixed to the satellite. The panels are mounted on frames that are linked together (9-14) and each link point has a pulley wheel (22-27) around which a continuous pulley cable passes.    The panels are arranged in a concertina fashion so that they can be folded into a flat stack when not in use. The pulley cables are covered in a plastic material that improves the thermal stability.    USE -   For space satellite solar panels.    ADVANTAGE -   Reduces sensitivity to temperature effects.    (DE19728844-C2)      The system includes solar panels (3-7) on a space satellite (1) supported on an out rigger that is fixed to the satellite. The panels are mounted on frames that are linked together (9- 14) and each link point has a pulley wheel (22-27) around which a continuous pulley cable passes.    The panels are arranged in a concertina fashion so that they can be folded into a flat stack when not in use. The pulley cables are covered in a plastic material that improves the thermal stability.    USE -   For space satellite solar panels.    ADVANTAGE -   Reduces sensitivity to temperature effects.    (JP11152098-A)      The system includes solar panels (3-7) on a space satellite (1) supported on an out rigger that is fixed to the satellite. The panels are mounted on frames that are linked together (9- 14) and each link point has a pulley wheel (22-27) around which a continuous pulley cable passes.    The panels are arranged in a concertina fashion so that they can be folded into a flat stack when not in use. The pulley cables are covered in a plastic material that improves the thermal stability.    USE -   For space satellite solar panels.    ADVANTAGE -   Reduces sensitivity to temperature effects.    (US6008447-A)      The system includes solar panels (3-7) on a space satellite (1) supported on an out rigger that is fixed to the satellite. The panels are mounted on frames that are linked together (9- 14) and each link point has a pulley wheel (22-27) around which a continuous pulley cable passes.    The panels are arranged in a concertina fashion so that they can be folded into a flat stack when not in use. The pulley cables are covered in a plastic material that improves the thermal stability.    USE -   For space satellite solar panels.    ADVANTAGE -   Reduces sensitivity to temperature effects.    (JP3175824-B2)      The system includes solar panels (3-7) on a space satellite (1) supported on an out rigger that is fixed to the satellite. The panels are mounted on frames that are linked together (9- 14) and each link point has a pulley wheel (22-27) around which a continuous pulley cable passes.    The panels are arranged in a concertina fashion so that they can be folded into a flat stack when not in use. The pulley cables are covered in a plastic material that improves the thermal stability.    USE -   For space satellite solar panels.    ADVANTAGE -   Reduces sensitivity to temperature effects.