Capture method of spacecraft capture system based on nozzle capture and star-rocket docking ring locking
A docking ring and spacecraft technology, which is applied to aerospace vehicles, aerospace vehicle docking devices, aircraft, etc., can solve the problems of poor versatility and adaptability of spacecraft capture systems, and achieve multiple reuse and economic benefits High, wide range of effects
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[0080] refer to image 3 The capture device 4 of this embodiment includes: an airbag storage mechanism 4-2, a locking airbag 4-3, a No. 1 global camera 4-4, three axial range finders 4-5, a buffer airbag 4-6, Transmission mechanism 4-7, gas supply system 4-8, three radial range finders 4-9, gas cylinder 4-10, attitude thruster 4-11, driving device 4-12, housing 4-13, propulsion Thrusters 4-14, controllers and docking devices 4-15.
[0081] Among them, the airbag storage mechanism 4-2 stores three locking airbags 4-3; the axial range finder 4-5 and the radial range finder 4-9 adopt a laser range finder; the attitude thruster 4-11 and the propulsion Thruster 4-14 adopts cold jet thruster.
[0082] Airbag storage mechanism 4-2, locking airbag 4-3, buffer airbag 4-6, transmission mechanism 4-7, air supply system 4-8, gas cylinder 4-10, driving device 4-12, housing 4- 13 form the airbag device;
[0083] The front end face of housing 4-13 is a conical surface, and buffer air bag...
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