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Configuration, for geostationary satellite mission
Configuration, for geostationary satellite mission
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机译：配置，用于对地静止卫星任务
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摘要
New configuration of the satellites avoiding the problem of limitation of the mass of the launcher. / p & & p & it is characterizes by a satellite of service is at least one power module 11 having solar panels 4 rigidly fasteners, and a control module 12 comprising a first unit 1 fixed to the power module 11 and arranged to be held pointee towards the sun, and a second unit 2 attachee to the first unit 1 by means of an interface device 3 for rotary pemettre to the second unit to be held pointee towards the earth. That - latter has at least one face 5 equiped of attachment means 7 for fastening at least one satellite payload 20 intended to be served and emerge from the satellite.
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