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Mission Design for the CubeSat OUFTI-1

Mission Design for the CubeSat OUFTI-1

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CHAPTER 88.4 Battery and operating modesAs above mentioned, no detailed study has been conducted over <strong>the</strong> powerhardware. Anyway, in analogy with all <strong>the</strong> o<strong>the</strong>r <strong>CubeSat</strong>s, launched or in anadvanced design phase, we will choose a lithium-ion battery because <strong>the</strong>y providemore energy per kilogram than o<strong>the</strong>r battery types. Regarding <strong>the</strong> powerconditioning and distribution unit, a non-regulated bus possibly coupled withDC/DC converters seems <strong>the</strong> best option.The lack of active attitude control and of a specific payload simplified <strong>the</strong> identificationsof operating modes respect to power. We have in fact only two operatingmodes depending on <strong>the</strong> D-STAR system. We have three elements requiringpower: <strong>the</strong> D-STAR system, <strong>the</strong> on board computer and <strong>the</strong> radio beacon. Thelatter, as introduced chapter 10, is <strong>the</strong> safer communications system and needsa power much smaller than that of D-STAR.Table 8.4: Operating modesMODE 1 MODE 1D-STAR OFF ONONBOARD COMPUTER ON ONRADIO BEACON ON ONThe first mode is a kind on stand-by mode: <strong>the</strong> on board computer is on and<strong>the</strong> radio beacon is sending <strong>the</strong> housekeeping data and receiving <strong>the</strong> commands.The second mode is <strong>the</strong> real operating mode when <strong>the</strong> D-STAR system is onand receiving and sending a amateur radio signal.Galli Stefania 84 University of Liège

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