Reusable flexible space debris capturing and despinning mechanism and use method
By using a flexible space debris capture and despinning mechanism, the problems of reusability, capture tolerance, and despinning when spacecraft capture space debris have been solved, achieving low-cost and efficient space debris capture and transfer.
Patent Information
- Authority / Receiving Office
- CN · China
- Patent Type
- Applications(China)
- Current Assignee / Owner
- BEIJING INST OF SPACECRAFT SYST ENG
- Filing Date
- 2026-01-30
- Publication Date
- 2026-04-28
AI Technical Summary
Existing spacecraft have problems when capturing space debris, such as non-reusability, small capture tolerance, high cost, and difficulty in eliminating the relative motion between the target and the spacecraft. They are particularly difficult to effectively capture non-cooperative targets with irregular shapes, spin, or nutation.
A flexible space debris capture and despinning mechanism was designed, comprising a distributed drive hatch mechanism, an deployable support mechanism, and a flexible storage bag. The hatch opening and closing and the support structure deployment and retraction are achieved through an eight-bar linkage and steel wire rope drive. Combined with the despinning brush inside the flexible storage bag, the space debris can be repeatedly captured and despinned.
It enables the repeated capture of space debris, reduces the overall weight and capture cost of spacecraft, improves capture tolerance, and effectively slows down the spin motion of debris through despin brushes, reducing its impact on the attitude of spacecraft.
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