12.07.2015 Views

Mission Design for the CubeSat OUFTI-1

Mission Design for the CubeSat OUFTI-1

Mission Design for the CubeSat OUFTI-1

SHOW MORE
SHOW LESS

Create successful ePaper yourself

Turn your PDF publications into a flip-book with our unique Google optimized e-Paper software.

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

Hooray! Your file is uploaded and ready to be published.

Saved successfully!

Ooh no, something went wrong!