| 摘要 |
A system and methods are disclosed for a modular platform configured to carry small payloads into orbit. The system comprises a prefabricated module comprising a plurality of panels. An orthogrid pattern can be located on an inner side of one or more of the panels. The orthogrid pattern can comprise an array of orthogonal recessed areas surrounded by an orthogrid wall. The system can include a bolt pattern comprising an attachment location placed near each corner of each recessed area. A torquer coil can be integrated into one or more of the panels.
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