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Mission Design for the CubeSat OUFTI-1

Mission Design for the CubeSat OUFTI-1

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CHAPTER4THE CUBESAT <strong>OUFTI</strong>-1<strong>OUFTI</strong>-1 is a <strong>CubeSat</strong> representing <strong>the</strong> first step of <strong>the</strong> LEODIUM Project:it’s also <strong>the</strong> first satellite of <strong>the</strong> University of Liège and <strong>the</strong> first Picosatelliteever made in Belgium. It’s an amateur radio satellite exploiting <strong>the</strong> digitalcommunicationD-STAR protocol and it’s not going to carry any scientific payloadbut it will mainly be used as a test <strong>for</strong> <strong>the</strong> D-STAR system into space: itcan be viewed as a bare-bone repeater in space.Fur<strong>the</strong>rmore, <strong>the</strong> <strong>OUFTI</strong>-1 bus could be used in <strong>the</strong> future as standard plat<strong>for</strong>m<strong>for</strong> <strong>the</strong> next <strong>CubeSat</strong>s of <strong>the</strong> University of Liège. As <strong>the</strong>y will have somescientific experiments on-board, <strong>the</strong> use of an already tested plat<strong>for</strong>m will allowto concentrate <strong>the</strong> ef<strong>for</strong>t on <strong>the</strong> payload and on <strong>the</strong> mission analysis in orderto reach <strong>the</strong> target in <strong>the</strong> best way as possible. Moreover, once <strong>the</strong> scientificmission will have finished, <strong>the</strong> <strong>CubeSat</strong> will be used by <strong>the</strong> amateur radio community:in return, we can communicate with <strong>the</strong> ground station trough <strong>the</strong>frequency bandwidth reserved <strong>for</strong> <strong>the</strong> amateur radio communications.The main constraint <strong>for</strong> this mission is <strong>the</strong> time line: <strong>the</strong> launch is in factscheduled <strong>for</strong> December 2008 and <strong>the</strong> project started in November 2007. Evenif two years are considered sufficient <strong>for</strong> <strong>the</strong> design and operation of a <strong>CubeSat</strong>mission, we need to optimize <strong>the</strong> time and to proceed as quickly as possible.For this reason we assumed <strong>the</strong> principle of KISS, Keep It Simple and Stupid.We are in fact convinced that between two possible solutions that guarantee <strong>the</strong>same final result, <strong>the</strong> most convenient is <strong>the</strong> simplest: guided by this idea, all<strong>the</strong> choices are taken in order to simplify <strong>the</strong> design.Be<strong>for</strong>e proceeding with <strong>the</strong> satellite description, an introduction to <strong>the</strong> <strong>CubeSat</strong>concept and to <strong>the</strong> D-STAR system is presented.19

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