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实用新型
CN205675262U 一种双单元立方体卫星平台 失效 - 放弃

一种双单元立方体卫星平台
摘要：
本实用新型公开了一种双单元立方体卫星平台，其包括主承力机构、迎风面电池阵、背风面电池阵、对天面电池阵、对地面电池阵、第一展开电池阵和第二展开电池阵和电路模块组，沿立方体卫星飞行方向，迎风面电池阵设置在主承力机构的迎风面上，背风面电池阵设置在主承力机构的背风面上，对天面电池阵设置在主承力机构的对天面上，对地面电池阵设置在主承力机构的对地面上，第一展开电池阵和第二展开电池阵分别设置在主承力机构的另外两个面上，电路模块组固定在主承力机构内。本实用新型有质量轻、体积小、成本低、研制周期短、功能密度高、应用广等显著优势。
摘要（英）：

The utility model discloses a two cell cube satellite platform, it includes primary load bearing mechanism, windward side battery battle array, lee side battery battle array, to sky face battery battle array, to ground battery battle array, first expansion battery battle array and second expansion battery battle array and circuit module group, along cube satellite flight direction, windward side battery battle array sets up on the windward side of primary load bearing mechanism, lee side battery battle array sets up on the lee side of primary load bearing mechanism, to sky face battery battle array set up primary load bearing mechanism to the sky face on, to ground battery battle array set up primary load bearing mechanism to subaerial, first expansion battery battle array and second expansion battery battle array set up respectively on two other faces of primary load bearing mechanism, circuit module group is fixed in primary load bearing mechanism. The utility model discloses have that the quality is light, small, with low costs, the leadtime is short, function density is high, use the advantage that is showing such as wide.

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