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Mission Design for the CubeSat OUFTI-1

Mission Design for the CubeSat OUFTI-1

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CHAPTER 5To conclude, we can say that with a footprint’s length of 3128 Km, <strong>OUFTI</strong>-1can cover <strong>the</strong> entire western Europe at once. Anyway, also at 350 Km altitudewith a footprint’s length of 1580 Km, <strong>the</strong> satellite passing over Paris can keep incontact an amateur radio operator in Lisbon with one in Stockholm. Concerning<strong>the</strong> Area Coverage Rate, it depends on <strong>the</strong> instrument dwell time and <strong>for</strong> anomnidirectional antenna it hasn’t any meaning.The Area Access Rate is estimated through <strong>the</strong> following <strong>for</strong>mula:AAR = 1.49 · 108 sin (λ)T5.6 Communication time={11660 Km2s6073 Km2s(1200Km)(350Km)(5.25)Directly connected to <strong>the</strong> earth coverage, we need to consider <strong>the</strong> communicationtime with <strong>the</strong> ground station in Liège. In fact, this is one of <strong>the</strong> drivingrequirements <strong>for</strong> <strong>the</strong> <strong>OUFTI</strong>-1 design. We are dealing with an amateur radiosatellite: as <strong>the</strong> community of amateur radio in almost uni<strong>for</strong>mly distributedall around <strong>the</strong> world, we chose to favor <strong>the</strong> Belgian amateur radio operators.In this way we also maximize <strong>the</strong> time available <strong>for</strong> communication with ourground station in Liège.But <strong>the</strong> same problem reappears in this case too: we cannot impose <strong>the</strong> orbitalparameters and specifically <strong>the</strong> argument of perigee and <strong>the</strong> right ascension onascending node. Hence we can only analyze <strong>the</strong> best and <strong>the</strong> worst situationand verify if <strong>the</strong> time is enough to satisfy <strong>the</strong> mission requirements.The worst case is represented in figure 5.6: as <strong>the</strong> perigee is over Belgium, <strong>the</strong>speed of <strong>OUFTI</strong>-1 passing over <strong>the</strong> ground station is extremely high and <strong>the</strong>time consequently really short.In <strong>the</strong> worst case we have an access time of 30 min/day. It seems to besufficient but this time is not continuous: <strong>the</strong> maximum continuous access timein <strong>the</strong> worst case is about 8 minutes.The best case is instead when <strong>the</strong> apogee is over Belgium and its representedin figure 5.6: in this case <strong>the</strong> time available <strong>for</strong> communication is much higheras <strong>the</strong> satellite is passing slowly over <strong>the</strong> ground station.In <strong>the</strong> best case we have an access time of 104 min/day with a maximumcontinuous time of 17 minutes.Galli Stefania 52 University of Liège

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