Mission Design for the CubeSat OUFTI-1
Mission Design for the CubeSat OUFTI-1
Mission Design for the CubeSat OUFTI-1
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CHAPTER 8Figure 8.5: Total power produced: simulation over one year orbit.Anyway, we are more interested in <strong>the</strong> power that we can effectively use at eachtime: we calculated <strong>the</strong>re<strong>for</strong>e <strong>the</strong> integrated power shown in figure 8.6. To haveit, we integrate <strong>the</strong> power over each orbit to have <strong>the</strong> total energy availableand <strong>the</strong>n we divided it by <strong>the</strong> orbit duration. In this way, we know exactly <strong>the</strong>power that we can guarantee continuously to our payload. All <strong>the</strong> losses on <strong>the</strong>electrical power system and in <strong>the</strong> battery haven’t been taken into account yet.Figure 8.6: Integrated power: simulation over one year orbitWe can see that, even in <strong>the</strong> worst period of <strong>the</strong> year, we can guarantee 1.3W. This is <strong>the</strong> value we will use to dimension our communication system.Galli Stefania 80 University of Liège