发明名称 CubeSat System, Method and Apparatus
摘要 A satellite system includes a chassis, an avionics package included within an upper portion of the chassis. The avionics package includes a main system board, a payload interface board, at least one daughter board and a battery board. The main system board, the payload interface board, the at least one daughter board, and the battery board reside in substantially parallel planes. The payload interface board, the at least one daughter board, and the battery board are coupled to the main system board through one or more stackable connectors. A method of operating a satellite is also described.
申请公布号 US2015039879(A1) 申请公布日期 2015.02.05
申请号 US201414517592 申请日期 2014.10.17
申请人 Cal Poly Corporation 发明人 Puig-Suari Jordi;Williams Austin
分类号 B64G1/66;G06F9/44 主分类号 B64G1/66
代理机构 代理人
主权项 1. A method for resetting a satellite comprising: selecting an interval for a long duration timer of between about one day and about 12 months; allowing the long duration timer to count down to zero; interrupting power to at least a portion of the satellite; and rebooting the at least one portion of the satellite.
地址 San Luis Obispo CA US