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en:assembly [2017/11/09 10:46]
rinin created
en:assembly [2020/03/25 16:28]
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-**Assembly** 
  
-{{ ru:​htmlimage.jpg?​direct&​200|}} 
-Structurally satellite model consists of a central cubic frame to which bodies of service modules and payload are mounted from inside or outside."​The Satellite"​ is hung to the rail with elastic tough nylon thread length from a meter to a meter and a half. The satellite has one degree of freedom to imitate zero gravity during the rotation around the vertical axis. 
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-**Note**: //the length of the thread is chosen from the condition of minimizing the impact to the cube's plane rotation. Bouncy rotational moment acting from the thread to the satelite still exists, but its impact is noticeable only when satellite twists several times. 
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-The central cube consists of four side panels, bottom and cover panels. Side panels have ledges, bottom and cover panels have corresponding mortises to arrange the panels relative to each other. The final positioning is carried out with help of corner blocks. 
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-On each panel there is a grid of screwed holes in 20 mm increments to attach modules to the central cube. The order of assembly, cabling and internal or external composition varies from the assigned task and is chosen by user. 
en/assembly.txt · Last modified: 2020/03/25 16:28 (external edit)