발사시 야기되는 랜덤진동을 고려한 위성체 전장품 설계 및 검증에 대한 연구

Design and Verification of Satellite Electronic Equipment with the consideration of Random Vibration while Launching

High level random vibration environments induced while launching of spacecraft can damage sensitive electronic equipment very rapidly, unless the equipment is properly packaged. Thus very careful consideration on the launch environment, especially for high level random vibration, is required in the design stage of electronic equipment of spacecraft. This paper describes the development process of Solar Array Regulator for KOMPAT-2, which is designed and tested by Korean engineers. Both analytical and experimental techniques are introduced in this paper.