12.07.2015 Views

Mission Design for the CubeSat OUFTI-1

Mission Design for the CubeSat OUFTI-1

Mission Design for the CubeSat OUFTI-1

SHOW MORE
SHOW LESS

Create successful ePaper yourself

Turn your PDF publications into a flip-book with our unique Google optimized e-Paper software.

CHAPTER 6.STRUCTURE AND DEPLOYMENTAll <strong>the</strong> systems have an operating temperature between -40 ◦ C and +85 ◦ C.The mass balance is reported in <strong>the</strong> following table:Table 6.1: <strong>CubeSat</strong> Kit massSkeletonized Mass [g] Solid-Walls Mass [g]Cover plate assembly 37 49Base plate assembly 50 62Main structure 71 132Chassis screws (x4) 2 2Total structure 166 251Flight module 50 50Total 216 301The skeletonized structure results much lighter than <strong>the</strong> solid-walls one.Even if <strong>the</strong> mass balance won’t be <strong>the</strong> most critical problem <strong>for</strong> <strong>OUFTI</strong>-1 because<strong>the</strong>re won’t be any added payload and we are not planning to use anyattitude control, we chose <strong>the</strong> skeletonized structure. In fact, one of <strong>the</strong> goals of<strong>the</strong> LEODIUM project is <strong>the</strong> development of a space plat<strong>for</strong>m that can be useby <strong>the</strong> future <strong>CubeSat</strong>s <strong>for</strong> scientific experiments: we have to make it as lighteras possible in order to have a greater mass available <strong>for</strong> payloads and attitudecontrol in <strong>the</strong> next missions, even if it wouldn’t be necessary <strong>for</strong> <strong>OUFTI</strong>-1.The main advantages of this structure is that we are sure of its reliability astwo <strong>CubeSat</strong>s are already flying with it: this is <strong>the</strong> key feature that make uschoose <strong>the</strong> <strong>CubeSat</strong>-Kit. The D-STAR system into space already represents infact a challenging technology demonstration, even if we haven’t any evidencethat it won’t correctly works: adding a possible structure failure to <strong>the</strong> alreadyexisting risks seemed us too much.Certainly some budget considerations have been done too, but <strong>the</strong>y have neverbeen <strong>the</strong> driving requirements.6.2 ISIS structureSince one and an half year, ISIS, Innovative Solution In Space (Delft, AL, TheNe<strong>the</strong>rlands), has developed a <strong>CubeSat</strong> structure based on <strong>the</strong> experience gainedwith <strong>the</strong> project of Delfi-C3. They also have some o<strong>the</strong>r products <strong>for</strong> <strong>CubeSat</strong>sand more in general <strong>for</strong> miniaturized satellites, as antennas and ground stationand <strong>the</strong>y provide a launch service.The structure is entirely made of an aluminium alloy 6061-T6 with <strong>the</strong> sideframesblack hard anodised and <strong>the</strong> ribs and shear-panels black alodyned.Galli Stefania 59 University of Liège

Hooray! Your file is uploaded and ready to be published.

Saved successfully!

Ooh no, something went wrong!