Mission Design for the CubeSat OUFTI-1
Mission Design for the CubeSat OUFTI-1
Mission Design for the CubeSat OUFTI-1
You also want an ePaper? Increase the reach of your titles
YUMPU automatically turns print PDFs into web optimized ePapers that Google loves.
CHAPTER 9A typical layout of a Thermal Excel sheet is in figure 9.4: this is <strong>the</strong> operatingcase with black coating. As expected <strong>the</strong> absorption function has been updated.Figure 9.4: Typical Thermal Excel layout: operating case whit black coatingIn <strong>the</strong> o<strong>the</strong>r sheets, <strong>the</strong> conductive and radiative equivalent resistance arepassed.As expected, <strong>the</strong> hottest face is <strong>the</strong> one directed towards <strong>the</strong> sun and <strong>the</strong> coldestthose watching only <strong>the</strong> cold space. The face pointing <strong>the</strong> earth is in an intermediatecondition. An interesting point is that <strong>the</strong> temperatures of solar cellsand structure on a same face are almost <strong>the</strong> same, even if <strong>the</strong>y seem equal. Forinstance, in black coated satellite in operating case we have <strong>for</strong> <strong>the</strong> face 1 <strong>the</strong>solar cell at 272.623 K and <strong>the</strong> structure at 272.624 K. Anyway, <strong>for</strong> all practicalcases, we can consider <strong>the</strong>m to be <strong>the</strong> same.In table 9.4 <strong>the</strong> results <strong>for</strong> different coatings and case are reported.Table 9.4: TemperaturesT0 MIN T INTERM T MAX TWHITE COLD CASE 236 K 236 K 236 K 236 KWHITE OPER. CASE 251 K 249.26 K 252.36 K 256.18 KWHITE HOT CASE 265.5 K 263.21 K 266.52 K 272.0 KBLACK COLD CASE 255 K 255 K 255 K 255 KBLACK OPER. CASE 275 K 272.62 K 276.13 K 283.60 KBLACK HOT CASE 287 K 284.04 K 287.83 K 296.99 KGOLD COLD CASE 266 K 266 K 266 K 266 KGOLD OPER. CASE 282 K 280.08 K 282.27 K 287.34 KGOLD HOT CASE 301.3 K 297.76 K 300.19 K 307.07 KWe can see that with a simple passive coating we can maintain <strong>the</strong> satellitetemperature within some reasonable limits.Galli Stefania 94 University of Liège