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Mission Design for the CubeSat OUFTI-1

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CHAPTER 8.POWER SYSTEMEectrons/cm 2 . For our mission <strong>the</strong> fluence over <strong>the</strong> lifetime, estimated through<strong>the</strong> software Spenvis, is of 8.55 · 10 11 : we can use <strong>the</strong> values of <strong>the</strong> third columneven if <strong>the</strong>y are too pessimistic.They give a value <strong>for</strong> <strong>the</strong> efficiency of 25.5 %: we will use 25% to be sure of notoversetimating <strong>the</strong> power.8.3 Power producedWe have now all <strong>the</strong> elements to calculate <strong>the</strong> power produced: <strong>the</strong> directionof sun rays, <strong>the</strong> eclipse duration and <strong>the</strong> solar arrays orientation. The programdeveloped calculates <strong>the</strong> eclipse’s anomalies of entrance and exit. Looping on<strong>the</strong> satellite anomaly, it determine whe<strong>the</strong>r it’s in sunlight or not: if yes, itcalculate <strong>the</strong> scalar product between <strong>the</strong> sun rays direction and <strong>the</strong> normal toeach face in order to have <strong>the</strong> incidence angle of sun:cos (β i ) = ˆN s · ˆN i i = 1 : 6 (8.11)where i indicates <strong>the</strong> face.If cos (β i ) < 0, it means that <strong>the</strong> face is not watching <strong>the</strong> sun as it’s turned in <strong>the</strong>opposite direction: it doesn’t contribute to <strong>the</strong> power production. O<strong>the</strong>rwisewe have <strong>the</strong> power produced by <strong>the</strong> i-th face:P i = C s A i η i cos (β i ) (8.12)As logical, <strong>the</strong> maximum power of a face is generated when <strong>the</strong> sun raysare perpendicular to it. This doesn’t mean that <strong>the</strong> total maximum power isproduced when one solar array is perpendicular <strong>the</strong> sun: in fact, in order tohave <strong>the</strong> total maximum power we need to add <strong>the</strong> contributions of all <strong>the</strong>faces. Indeed, <strong>the</strong> Delfi-C3 team per<strong>for</strong>med a study to optimize <strong>the</strong> orientationof solar cells: it came out that <strong>the</strong> best configuration is when a corner is directedto <strong>the</strong> sun.Once we have <strong>the</strong> power generated by each face, we sum <strong>the</strong> contribution andwe have <strong>the</strong> total power.8.3.1 Elliptic orbit with starting orbital elementsFor <strong>the</strong> <strong>OUFTI</strong>-1 elliptical orbit in case of Ω = 0, ω = 0 and <strong>for</strong> a simulationstarting at <strong>the</strong> vernal equinox we have <strong>the</strong> result represented in figure 8.5.Each vertical line represents one orbit on <strong>the</strong> moment of <strong>the</strong> year indicatedby <strong>the</strong> earth anomaly in abscissa. In blue are represented <strong>the</strong> eclipses and in<strong>the</strong> dark red <strong>the</strong> maximum power.Galli Stefania 79 University of Liège

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