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- W3142020227 abstract "In view of the drawbacks of the currently used pico-satellite deployers,a new cage style deployer was put forward,which is characteristic of cutter unlocking the door,conical spring driving the pico-satellite,oriented rail restricting the direction,cam controlling the start movement of pico-satellite,locking shaft fixing the door and having power supply system itself.This structure greatly reduces the constraint on the pico-satellite design,and avoids the collision or scratch between the pico-satellite and the deployer door.The design also reduces the dependence on the rocket and greatly increases its compatibility with the rocket.In this work,the deployer research includes designing,theoretical calculation of the deploying process and experimental verification.The results of calculation and experiment show that the design can meet the requirements fully,including the mass of the deployer,deploying velocity,overload of the axial direction and the transverse direction and basic frequency.This can be regarded as reference for the further development." @default.
- W3142020227 created "2021-04-13" @default.
- W3142020227 creator A5035193825 @default.
- W3142020227 date "2014-01-01" @default.
- W3142020227 modified "2023-09-24" @default.
- W3142020227 title "New cage style pico-satellite deployer based on sliding guide structure" @default.
- W3142020227 hasPublicationYear "2014" @default.
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