PURPOSE: A hinge apparatus and a satellite having the same are provided to ensure development reliability in a simple structure wherein hinge brackets supporting the satellite body and a solar panel are connected with elastic members. CONSTITUTION: A first hinge bracket(40) is installed in a first unit. A second hinge bracket(50) is installed in a second unit. A connector(60) interlinks the first and second hinge brackets. The connector creates a restoring force in a folded state where the first and second units are faced each other. A coil spring is provided in the connector to gradually reduce the restoring force in the same direction as the second unit is opened with respect to the first unit.
申请公布号
KR20100020228(A)
申请公布日期
2010.02.22
申请号
KR20080078921
申请日期
2008.08.12
申请人
KOREA AEROSPACE RESEARCH INSTITUTE
发明人
KIM, KYUNG WON;KIM, SUN WON;LIM, JAE HYUK;RHEE, JU HUN;HWANG, DO SOON;SONG, WOON HYUNG;CHOI, HANG SUK;KIM, JIN HEE;JIN, IK MIN;KIM, HAK JUNG