.Deployment structure restraint device for satellites with active wire tension control

摘要

The present invention relates to a device for constraining a deployment structure for a satellite having an active wire tension control function, and more particularly, it is possible to restrain the deployment structure to the body of the satellite by winding the wire in a dial lock method to generate tension. And, it relates to a constraining device for a deployment structure for a satellite having an active wire tension control function capable of maintaining tension by actively winding the wire even when the wire is fired and stretched in a vibrating environment.