Mission Design for the CubeSat OUFTI-1
Mission Design for the CubeSat OUFTI-1 Mission Design for the CubeSat OUFTI-1
CHAPTER 5Figure 5.6: Vega: spacecraft hazardous operations phase2. Combined operationsIt includes the spacecraft integration on the adapter and installation insidethe fairing, the verification procedures and the transfer to the launch pad.Galli Stefania 30 University of Liège
CHAPTER 5.MISSION ANALYSISFigure 5.7: Vega: combined operations phase3. Launch countdownIt covers the last launch preparation sequence up to the lift-off.Galli Stefania 31 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
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- 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
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- 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 and 46: CHAPTER 5.MISSION ANALYSISwhere ϑ
- Page 47 and 48: CHAPTER 5.MISSION ANALYSISFigure 5.
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- 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
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- 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
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CHAPTER 5.MISSION ANALYSISFigure 5.7: Vega: combined operations phase3. Launch countdownIt covers <strong>the</strong> last launch preparation sequence up to <strong>the</strong> lift-off.Galli Stefania 31 University of Liège
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