Mission Design for the CubeSat OUFTI-1

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CHAPTER 5Figure 5.18: Eccentricity variation over a year.Figure 5.19: Perigee and apogee altitude variation over a year.Galli Stefania 46 University of Liège
CHAPTER 5.MISSION ANALYSISFigure 5.20: Inclination variation over a year.Figure 5.21: Right ascension of ascending node variation over a yearGalli Stefania 47 University of Liège
Page 3: Space is probably the main symbol o
Page 7 and 8: CONTENTS1 Introduction 132 The LEOD
Page 9 and 10: LIST OF FIGURES4.1 A typical 1-unit
Page 11: LIST OF TABLES5.1 Comparison betwee
Page 15 and 16: CHAPTER2THE LEODIUM PROJECTThe LEOD
Page 17: CHAPTER3THE FLIGHT OPPORTUNITYThe E
Page 20 and 21: CHAPTER 44.1 The CubeSat conceptDur
Page 22 and 23: CHAPTER 4have to be smooth and thei
Page 25 and 26: CHAPTER5MISSION ANALYSISThe mission
Page 27 and 28: CHAPTER 5.MISSION ANALYSIS5.1.1 Typ
Page 29 and 30: CHAPTER 5.MISSION ANALYSISIt can be
Page 31 and 32: CHAPTER 5.MISSION ANALYSISFigure 5.
Page 33 and 34: CHAPTER 5.MISSION ANALYSIS5.2 The o
Page 35 and 36: CHAPTER 5.MISSION ANALYSIS• the s
Page 37 and 38: CHAPTER 5.MISSION ANALYSISt − t 0
Page 39 and 40: CHAPTER 5.MISSION ANALYSISIn figure
Page 41 and 42: CHAPTER 5.MISSION ANALYSIS• if m
Page 43 and 44: CHAPTER 5.MISSION ANALYSIS5.3.3 The
Page 45: CHAPTER 5.MISSION ANALYSISwhere ϑ
Page 49 and 50: CHAPTER 5.MISSION ANALYSISA four ye
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 and 104:
CHAPTER 10.COMMUNICATION SYSTEMWe c
Page 105 and 106:
CHAPTER11TESTSThe launch and space
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
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Mission Design for the CubeSat OUFTI-1

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