The invention discloses a space junk removal
satellite device which comprises a
satellite body and a task execution module. The
satellite body comprises a first structure box, a
power module, a navigation module, an
orbit control module, a flight control module, a
wireless communication module and a
solar cell array, the
power module, the navigation module, the
orbit control module, the flight control module and the
wireless communication module are arranged in the first structure box, the first structure box is a cube, and all the faces of the box are fixed through mechanical structures; andthe task execution module comprises a second structure box, a
task control module, a detection recognition module, a capture module, a smashing module, a transporting module and a
laser ablation module, the
task control module, the detection recognition module, the capture module, the smashing module, the transporting module and the
laser ablation module are arranged in the second structure box, the second structure box is a cube, the left side face of the second structure box is a fixed face mechanically locked to the satellite body, and the remaining five faces are each of a deformable structure and can be unfolded and folded within the range from -60 degrees to 60 degrees. The device can capture and remove small-size space junk, and the space junk containing a conductive material can beablated through the
laser ablation module and then secondarily used to
supply energy to the
laser ablation module.