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Mission Design for the CubeSat OUFTI-1

Mission Design for the CubeSat OUFTI-1

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CHAPTER 55.1 The Vega LauncherVega, Vettore Europeo di Generazione Avanzata, is <strong>the</strong> new European smalllauncher. It has been designed as a single body launcher with three solidpropulsion stages and an additional liquid propulsion restartable upper module,AVUM, used <strong>for</strong> attitude and orbit control and <strong>for</strong> satellite release. Unlikemost small launchers, Vega will be able to place multiple payloads into orbit.Its development started in 1998 and <strong>the</strong> first flight was initially expected in2007 from <strong>the</strong> Guyana Space Center, CSG, but different reasons causes somedelays and, up to know, it is scheduled <strong>for</strong> <strong>the</strong> December 2008.It is funded by Belgium, France, Italy, Spain, Sweden, Switzerland and TheNe<strong>the</strong>rlands.Vega is 30 m high, has a maximum diameter of 3 m and weights 137 tons atlift-off. As shown in fig.5.1, it has three sections: <strong>the</strong> Lower Composite, <strong>the</strong>Upper Composite known as AVUM and <strong>the</strong> Payload Composite.Figure 5.1: Vega launcherGalli Stefania 26 University of Liège

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