SATELLITE FOR DEPLOYMENT APPARATUS USING TAPE SPRING HINGE AND COIL SPRING HINGE

摘要

The present invention, regarding a deployment apparatus for a satellite which is installed between solar panels, and deploys by changing an angle between the solar panels, relates to a deployment apparatus for a satellite using a tape spring hinge and a coil spring hinge, comprising: a plurality of tape spring hinges formed in a height direction; a coil spring hinge arranged as interposed between the tape spring hinges; and connection members which are respectively installed at both ends of the tape spring hinge and the coil spring hinge and connect the solar panels.