| 摘要 |
PROBLEM TO BE SOLVED: To obtain a wiring structure suppressing wire breaking and effects on signal wires due to increase in internal temperature accompanied by lashing of a wire harness inside a satellite. SOLUTION: A plurality of screw holes 73 are provided along the longitudinal direction at predetermined intervals, and busbars 50 for positive power supply and negative power supply are parallelly connected on a body structure panel 4 on an inner face of a satellite body structure. The busbar 50 comprises a conductor 53 and an insulator 54 covering the periphery of the conductor 53. The wire harness 110 formed by binding a plurality of electric power lines is connected to the screw hole 73 of the busbar 50 to supply electric power to electronic equipment mounted on the satellite. COPYRIGHT: (C)2007,JPO&INPIT
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