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Mission Design for the CubeSat OUFTI-1

Mission Design for the CubeSat OUFTI-1

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CHAPTER 99.1 Passive <strong>the</strong>rmal-controlThe <strong>the</strong>rmal control of <strong>OUFTI</strong>-1 is a critical problem. In fact, as <strong>the</strong> satellite isnot-stabilized, we need to place solar cells on each face and, if we want enoughpower, we need <strong>the</strong>ir surface to be as big as possible: <strong>the</strong> place available <strong>for</strong><strong>the</strong>rmal control surfaces is really small. Anyway with an accurate choice of <strong>the</strong>coating material we still can guarantee <strong>the</strong> respect of temperature limits.We chose a passive control system based on painting: we need <strong>the</strong>re<strong>for</strong>e tochoose a coating and to verify that <strong>the</strong> limits are respected.The <strong>the</strong>rmal equilibrium depends on <strong>the</strong> incoming and outgoing heat flux. Makingit on a satellite means to consider <strong>the</strong> spacecraft, <strong>the</strong> sun, <strong>the</strong> earth and <strong>the</strong>cold space. Basing on <strong>the</strong> Wien’s law, each body radiates mainly at a wavelengthwhich depends on its temperature: looking <strong>the</strong> temperatures of all thisbodies, we notice that <strong>the</strong> radiative exchanges are mainly at visible and infraredwavelength. Fur<strong>the</strong>rmore <strong>the</strong> Kirchhoff <strong>the</strong>orem says that <strong>the</strong> spectral directionalemissivity and absorption have <strong>the</strong> same value. Extending this <strong>the</strong>oremto <strong>the</strong> integrated absorption and emissivity, ESA and NASA adopted <strong>the</strong>re<strong>for</strong>ea special convention: <strong>the</strong>y call ɛ <strong>the</strong> absorption and emissivity factor in infraredand α <strong>the</strong> absorption and emissivity factor in visible.α = α V IS = ɛ V ISɛ = α IR = ɛ IRWe will use this rule.As <strong>the</strong> incoming flux is mainly visible and <strong>the</strong> outgoing infrared, <strong>the</strong> equilibriumtemperature of a body in space depends from <strong>the</strong> ratio α : <strong>the</strong> higher this ratio,ɛ<strong>the</strong> warmer <strong>the</strong> body.Doing passive <strong>the</strong>rmal control based on painting means to choose <strong>the</strong> appropriatecolor to keep <strong>the</strong> body temperature within its limits. If we have a body inspace without any kind of power production on board and we neglect <strong>the</strong> earth,<strong>the</strong> <strong>the</strong>rmal balance says:C s Aα = AɛσT 4 (9.1)where C s is <strong>the</strong> solar constant and σ = 5.67 · 10 −8 WBoltzmann constant.Hence we can obtain <strong>the</strong> equilibrium temperature as:m 2 Kis <strong>the</strong> Stefan-√4T eq∼ Cs α = (9.2)σɛIn table 9.1 <strong>the</strong> value of α end ɛ and of <strong>the</strong> equilibrium temperature <strong>for</strong> threecolors are reported.We see that if we want to have a cold satellite we can paint it in white, o<strong>the</strong>rwisewe can choose between black and golden, depending on <strong>the</strong> temperaturewe would like to reach.Galli Stefania 86 University of Liège

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