DEPLOYMENT TEST FOR SOLAR PANEL OF SATELLITE

摘要

The present invention relates to a test apparatus for a satellite solar panel, the configuration of which is possible to hinge the body dummy 70, the solar panel dummy 80, the body dummy 70 and the solar panel dummy 80. A hinge means (90) for connecting, and a deployment means (110) provided between the main body stack (70) and the solar panel stack (80) to move the solar panel stack (80) from a folded position to a deployed position. Satellite dummy portion including; The first horizontal frame 210 in which the main body dummy 70 is seated, and the second horizontal panel 210 in which the solar panel dummy 80 positioned in an deployed position at an angle with the first horizontal frame 210 is seated A main frame part 200 including a horizontal frame 220; A torque measuring unit 300 for measuring torque generated when the solar panel dummy 80 moves from a folded position to a deployed position; A force measurement unit provided at a portion where the main body dummy 70 and the deployment means 110 are connected to measure the force applied to the deployment means 110 when the solar panel dummy 80 is positioned at the deployment position. (400); according to the above configuration, by testing using a satellite dummy portion having the same mechanical properties as the actual satellite, it is possible to expect the effect of cost reduction without being significantly limited by space.