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公开(公告)号:KR1020100018839A
公开(公告)日:2010-02-18
申请号:KR1020080077534
申请日:2008-08-07
Applicant: 한국항공우주연구원
Abstract: PURPOSE: An NEA unit and the deployment test device of a satellite solar array including the same are provided to manufacture the NEA unit simply with a low cost by manufacturing the NEA unit fixing and releasing the solar array with an electromagnet. CONSTITUTION: A fixing part is included on the side of a hinged solar array. A electromagnet part(152) fixes and releases the hinged solar array by optionally combining to the fixing part. A housing(151) receives the electromagnet part. The electromagnet part includes a controller and a rectifier for supplying power. A part of the side of the housing is opened to forms a first opening part(512). A cover plate(153) is formed to close the first opening.
Abstract translation: 目的:提供NEA单元和包括其的卫星太阳能阵列的部署测试装置,通过制造NEA单元来简单地以低成本制造NEA单元,并用电磁铁固定和释放太阳能阵列。 构成:固定部件包括在铰接太阳能阵列的一侧。 电磁铁部件152通过可选地组合到固定部件来固定和释放铰接的太阳能电池阵列。 壳体(151)接收电磁体部分。 电磁铁部件包括用于供电的控制器和整流器。 壳体侧面的一部分被打开以形成第一开口部分(512)。 形成盖板(153)以封闭第一开口。
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公开(公告)号:KR100986002B1
公开(公告)日:2010-10-06
申请号:KR1020080077534
申请日:2008-08-07
Applicant: 한국항공우주연구원
CPC classification number: B64G7/00
Abstract: PURPOSE: An NEA unit and the deployment test device of a satellite solar array including the same are provided to manufacture the NEA unit simply with a low cost by manufacturing the NEA unit fixing and releasing the solar array with an electromagnet. CONSTITUTION: A fixing part is included on the side of a hinged solar array. A electromagnet part(152) fixes and releases the hinged solar array by optionally combining to the fixing part. A housing(151) receives the electromagnet part. The electromagnet part includes a controller and a rectifier for supplying power. A part of the side of the housing is opened to forms a first opening part(512). A cover plate(153) is formed to close the first opening.
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