| 摘要 |
The invention relates to a deployment system for spatial appendages for example solar generators, comprising at least one two-phase deployment articulation line, furnished with two rotation spindles (10, 20). According to the invention the deployment system comprises a synchronization mechanism (101, 102, 103, 106, 107) for the two rotation spindles so that when the driving spindle (20) rotates during a first deployment phase, the driven spindle (10) does not rotate, and then, when the driving spindle rotates during the second deployment phase, the driven spindle rotates in a manner synchronized with the driving spindle.
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