| 摘要 |
The invention relates to a variable-angle locking mechanism for a spacecraft. The mechanism includes a mobile part (20) mounted so as to pivot on a fixed part (26) and carrying a fastening element (10) which can be locked with a locking element (31) mounted so as to pivot on the fixed part (26). The locking element can be positioned linearly on the mobile part by a single wedge (30), the thickness of which determines the deployment angle of the mobile element. Field of application: adjusting the deployment of solar panels on spacecraft, etc. <IMAGE> |
