The application discloses a pointing mirror
assembly and a bonding tool thereof, and relates to the technical field of space
laser communication. The pointing mirror adopts a back convex cylindrical structure form, improves the rigidity of the bonding part of the mirror body, improves the anti-deformation capability, and provides sufficient operation space for the tool at the back. The flexible joint is locally bonded with the mirror body, and a force releasing lever is formed from the bonding point to the inner flexible groove root, so that the shrinkage deformation of the glue layer is released, the bonding stress is reduced, and the bonding stress caused by the continuous bonding of the whole circumference of the outer cylindrical surface is avoided. In addition, the circumferential material of the bonding point is continuous, the bonding surface cylindricity and local rigidity are easy to control, the uniformity of the glue layer is easy to guarantee, and the pointing mirror position stability under vibration is stable. The external interfaces are far away from each other, and the unevenness influence is weakened. By selecting appropriate bonding
layer thickness adhesive and using the tool plug, the two bonding parts do not need to be precisely machined and matched. After bonding, the
assembly precision and consistency are high, the subsequent whole
machine adjustment is facilitated, and the
space environment working condition requirements are met.