The invention discloses a cuboid satellite orbit deployer. The cuboid satellite orbit deployer comprises a top plate, a base plate, two opposite side plates, a back plate, a cabin door arranged opposite to the back plate, a main spring and the like; the deployer forms a totally-sealed cuboid cagelike structure, the inside of the deployer is used for loading a cuboid satellite, the main spring is arranged on the back plate, and a push plate is arranged in the cagelike structure of the deployer. A door frame is fixed to the top plate, the base plate and the side plates. The main spring is in a state of compression after loading of the cuboid satellite, the satellite abuts against the push plate at the moment, the cabin door opens when the orbit is deployed, the main spring and the push plate together drive the cuboid satellite to be popped, wherein a cabin door opening mechanism is controlled by electromagnetism, by the corporation of a permanent magnet and a direct-current electromagnetic coil, the opening of the cabin door is achieved under the action of a cabin door spring arranged at the bottom of the door frame.
Cuboid satellite orbit deployer
2015-06-24
Patent
Electronic Resource
English
IPC: | B64G Raumfahrt , COSMONAUTICS |