Mission Design for the CubeSat OUFTI-1
Mission Design for the CubeSat OUFTI-1 Mission Design for the CubeSat OUFTI-1
CHAPTER 10failure reasons. It’s also true that, without the D-STAR system, OUFTI-1 willbe useless as inaccessible by the amateur radio community: all the tests will betherefore performed to avoid such a kind of problem.Concerning the ground station, it will be installed in the University of Liègearea. It will be a traditional tracking station for simultaneous transmission andreception on the amateur radio frequencies and it will be connected with thealready existing D-STAR repeater of the university to exploit all the systemproperties, included the connection to the internet. A backup ground stationwill also be installed in the neighborhood: it main purpose is to track othersatellites but it can be used for OUFTI-1 if needed.A possible participation of this ground station to the GENSO (Global EducationalNetwork for Satellite Operations) network is also wished.Galli Stefania 104 University of Liège
CHAPTER11TESTSThe launch and space environment are extremely hard for the spacecraft: it isin fact subject to vibrations at different frequencies, vacuum and frequent thermalcycling. Given that, once in orbit, there is not any way to repair a damageon the satellite, we need to verify that all the components and the integratedsystem can survive to the external environment: the block of all these actionsconstitutes the test campaign. The tests usually performed on a satellite beforelaunch include mechanical test as vibrations and shocks, environmental tests asthermal vacuum and functional test as the electromagnetic compatibility. Thetests level and duration depends, on the one hand, on the test philosophy and,on the other hand, on the launcher specifications and on the space environmentexpected. We can then demonstrate some spacecraft function by testing somegroup on components: it is called verification test and typically includes theantennas and solar arrays deployment test.105
- Page 53 and 54: CHAPTER 5.MISSION ANALYSISFigure 5.
- Page 55: CHAPTER 5.MISSION ANALYSISFigure 5.
- Page 58 and 59: CHAPTER 66.1 Pumpkin structureThe s
- Page 60 and 61: CHAPTER 6Figure 6.2: ISIS structure
- Page 62 and 63: CHAPTER 6Figure 6.3: P-POD: deploym
- Page 64 and 65: CHAPTER 77.1 Inertia propertiesBefo
- Page 66 and 67: CHAPTER 7I x = I x,cube + I x,M + I
- Page 68 and 69: CHAPTER 7This rough estimation is e
- Page 70 and 71: CHAPTER 7Otherwise, an orbit simula
- Page 72 and 73: CHAPTER 7only slow down the rotatio
- Page 74 and 75: CHAPTER 8order to prevent any failu
- Page 76 and 77: CHAPTER 8We have now the vector ˆN
- Page 78 and 79: CHAPTER 8Here we add an important h
- Page 80 and 81: CHAPTER 8Figure 8.5: Total power pr
- Page 82 and 83: CHAPTER 8Figure 8.8: Total power an
- Page 84 and 85: CHAPTER 88.4 Battery and operating
- Page 86 and 87: CHAPTER 99.1 Passive thermal-contro
- Page 88 and 89: CHAPTER 99.3 Nodes modelThe CubeSat
- Page 90 and 91: CHAPTER 9where c p is the material
- Page 92 and 93: CHAPTER 9We have now all the parame
- Page 94 and 95: CHAPTER 9A typical layout of a Ther
- Page 97 and 98: CHAPTER10COMMUNICATION SYSTEMThe co
- Page 99 and 100: CHAPTER 10.COMMUNICATION SYSTEMstre
- Page 101 and 102: CHAPTER 10.COMMUNICATION SYSTEM•
- Page 103: CHAPTER 10.COMMUNICATION SYSTEMWe c
- Page 107 and 108: CHAPTER 11.TESTSof asking for some
- Page 109 and 110: CHAPTER 11.TESTSThe random vibratio
- Page 111 and 112: CHAPTER12FUTURE DEVELOPMENTSThe fea
- Page 113: CHAPTER 12.FUTURE DEVELOPMENTSspace
- Page 117 and 118: AcronymsAARACRACSADADCSASIAVUMBOLCC
- Page 119 and 120: BIBLIOGRAPHY[1] Wiley J. Larson, Ja
- Page 121: AcknowledgmentsI would like to than
CHAPTER 10failure reasons. It’s also true that, without <strong>the</strong> D-STAR system, <strong>OUFTI</strong>-1 willbe useless as inaccessible by <strong>the</strong> amateur radio community: all <strong>the</strong> tests will be<strong>the</strong>re<strong>for</strong>e per<strong>for</strong>med to avoid such a kind of problem.Concerning <strong>the</strong> ground station, it will be installed in <strong>the</strong> University of Liègearea. It will be a traditional tracking station <strong>for</strong> simultaneous transmission andreception on <strong>the</strong> amateur radio frequencies and it will be connected with <strong>the</strong>already existing D-STAR repeater of <strong>the</strong> university to exploit all <strong>the</strong> systemproperties, included <strong>the</strong> connection to <strong>the</strong> internet. A backup ground stationwill also be installed in <strong>the</strong> neighborhood: it main purpose is to track o<strong>the</strong>rsatellites but it can be used <strong>for</strong> <strong>OUFTI</strong>-1 if needed.A possible participation of this ground station to <strong>the</strong> GENSO (Global EducationalNetwork <strong>for</strong> Satellite Operations) network is also wished.Galli Stefania 104 University of Liège