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Mission Design for the CubeSat OUFTI-1

Mission Design for the CubeSat OUFTI-1

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CHAPTER 99.3 Nodes modelThe <strong>CubeSat</strong> configuration is still unknown and <strong>the</strong>re<strong>for</strong>e a precise <strong>the</strong>rmalstudy is impossible. The best thing to do in this case is to generate an equivalentnodes model in order to have a simplified representation of <strong>the</strong> structure to verify<strong>the</strong> <strong>the</strong>rmal exchanges with an equivalent electric model. Then <strong>the</strong> model ispassed to Thermal Excel. The fist step is indeed to identify a representationthat well symbolize <strong>the</strong> satellite: this corresponds to choose where to place <strong>the</strong>nodes. Then we need to identify <strong>the</strong> resistive connection between <strong>the</strong> nodesbased on <strong>the</strong> properties of <strong>the</strong> modeled part. In <strong>the</strong> next paragraphs this twosteps will be treated.9.3.1 RepresentationThe idea is to place a node <strong>for</strong> each part of <strong>the</strong> satellite and to study its <strong>the</strong>rmalbehavior in <strong>the</strong> steady-state case: <strong>the</strong> model is shown in figure 9.1We assume that <strong>the</strong>re is a face watching <strong>the</strong> earth and one directed to sun.Each face is represented by two nodes: <strong>the</strong> <strong>the</strong>rmal coating and <strong>the</strong> solar cell (wehave two solar cells but <strong>the</strong>y are modeled as one node). The solar cells are <strong>the</strong>nlinked to <strong>the</strong> back face structure through an equivalent conductive resistance.As <strong>the</strong> <strong>the</strong>rmal coating thickness is really small, we consider it as a part of<strong>the</strong> structure: basically we use <strong>the</strong> conductive parameters of <strong>the</strong> real aluminumalloy material but <strong>the</strong> optics coefficient of <strong>the</strong> coating <strong>for</strong> <strong>the</strong> radiation. Thishypo<strong>the</strong>sis is equivalent to impose that <strong>the</strong> coating and <strong>the</strong> back face structurehave <strong>the</strong> same temperature: as <strong>the</strong> <strong>the</strong>rmal coating is just a painting, this isdefinitely verified in <strong>the</strong> reality. The node corresponding to <strong>the</strong> face structureis <strong>the</strong>n connected to <strong>the</strong> o<strong>the</strong>r faces trough a conductive resistance.With reference to figure 9.1 we have <strong>the</strong> following convection:• nodes 1 → 6 are <strong>the</strong> solar cells• nodes 7 → 12 are <strong>the</strong> faces structures with <strong>the</strong>rmal coating• node 99 is <strong>the</strong> cold space• node 98 is <strong>the</strong> earth• <strong>the</strong> black resistances represent conduction between solar cells and structure.They are based on solar cells properties• <strong>the</strong> blue resistances represent conduction between faces. They are basedon structure properties• <strong>the</strong> red resistances represent <strong>the</strong> infrared radiation between <strong>the</strong> faces and<strong>the</strong> cold space. They are based on surface properties.Galli Stefania 88 University of Liège

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