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CubeSat Separation Parameter Optimization

Published • Dec 1, 2018
NobleIDNI1P86W95R24S84
Authors:
Jiaolong Zhang
,
Zhou Jun
,
Yaosheng Deng

Abstract

To implement noninterference deployment and meet the initial orbital attitude requirements of CubeSat, the CubeSat separation process is designed, theoretical analyzed and parameter optimized. Aiming at the direct-driving kinematic scheme of separation spring pushing CubeSat to open the door, the dy...

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