Mission Design for the CubeSat OUFTI-1

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CHAPTER 13SEPSEUSPENVISSRSSSOVEGASingle Event PhenomenaSingle Event UpsetSPace ENVironment Information SystemShock Response SpectrumSun Synchronous OrbitVettore Europeo di Generazione Avanzata(European Vehicle of Advanced Generation)Galli Stefania 118 University of Liège
BIBLIOGRAPHY[1] Wiley J. Larson, James R. Wertz, Space Mission Analysis and Design,third ed., Springer, Space Technology Library, 1999[2] James R. Wertz, Spacecraft Attitude Determination and Control, Springer,Space Technology Library, 1978[3] Vladimir A. Chobotov, Orbital Mechanics, American Institute of Aeronauticsand Astronautics, 2002[4] James R. Wertz, Mission Geometry Orbit and Constellation Design Management,Springer, Space Technology Library, 2001[5] P. Rochus, V. Rochus, Contrôle thermique spatial, notes of Conceptiond’expériences spatiales classes, University of Liège[6] P. Rochus, Effet de l’environnement spatial sur la conception, notes ofConception d’expériences spatiales classes, University of LiègeAPPLICABLE DOCUMENTS[AD1] Vega User’s Manual, Issue 3, Rev. 0, March 2006[AD2] Vega Launch Vehicle Program General Specification: Qualification andAcceptance Test of Equipments (VG-SG-1-C-040-SYS), Issue 5, Rev. 1, 13November 2006[AD3] Poly Picosatellite Orbital Deployer Interface Control Document, Issue 1,11 February 2004[AD4] CubeSat Design Specification, Rev. 10, 2 August 2006[AD5] Cubesat P-POD Deployer Requirements, May 2002REFERENCE DOCUMENTS119
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Space is probably the main symbol o
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CONTENTS1 Introduction 132 The LEOD
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LIST OF FIGURES4.1 A typical 1-unit
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LIST OF TABLES5.1 Comparison betwee
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CHAPTER2THE LEODIUM PROJECTThe LEOD
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CHAPTER3THE FLIGHT OPPORTUNITYThe E
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CHAPTER 44.1 The CubeSat conceptDur
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CHAPTER 4have to be smooth and thei
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CHAPTER5MISSION ANALYSISThe mission
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CHAPTER 5.MISSION ANALYSIS5.1.1 Typ
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CHAPTER 5.MISSION ANALYSISIt can be
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CHAPTER 5.MISSION ANALYSISFigure 5.
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CHAPTER 5.MISSION ANALYSIS5.2 The o
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CHAPTER 5.MISSION ANALYSIS• the s
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CHAPTER 5.MISSION ANALYSISt − t 0
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CHAPTER 5.MISSION ANALYSISIn figure
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CHAPTER 5.MISSION ANALYSIS• if m
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CHAPTER 5.MISSION ANALYSIS5.3.3 The
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CHAPTER 5.MISSION ANALYSISwhere ϑ
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CHAPTER 5.MISSION ANALYSISA four ye
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CHAPTER 66.1 Pumpkin structureThe s
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CHAPTER 6Figure 6.2: ISIS structure
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CHAPTER 6Figure 6.3: P-POD: deploym
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CHAPTER 77.1 Inertia propertiesBefo
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CHAPTER 7I x = I x,cube + I x,M + I
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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
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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
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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
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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: AcronymsAARACRACSADADCSASIAVUMBOLCC
Page 121: AcknowledgmentsI would like to than
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Mission Design for the CubeSat OUFTI-1

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