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Releases: oresat/oresat-structure

Struts as Heat Spreaders

29 Jan 08:49
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Pre-release

This is a stable release. By that, I mean that there are no errors in the top-level assembly.

The struts from the +X face have been added to all frames. The intent is that the solar panels will be thermal-epoxied to the struts to dump solar heat.

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vibration/weight enhancements

13 Jan 01:49
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Pre-release

This is (approximately) just before the 2018 antenna capstone started working on OreSat.

  • This keeps the same form factor as previous versions.
  • It uses far fewer fasteners to attach the +/-Y frames to the -X frame (total of 4).
  • It avoids (in all cases) putting fasteners on the same slot that a solar panel or backplane screw hole sits on. Thus, all holes (except for the counter-bores) may be drilled as through holes.
  • The +/-Y frames also now have slots cut out to reduce mass.
  • The slots for the cards no longer create 0.4 mm thin features. (It's now 1 mm.)
  • The +X frame now features hold-down beams, which prevent the +X sides of the cards from vibrating by holding them with slots similar to those on the +/-Y frames.

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SolidWorks migration

13 Jan 02:00
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SolidWorks migration Pre-release
Pre-release

This is the state of the model after migrating back form STEP to SolidWorks. It is essentially the same as v0.5.

v0.4

18 May 17:18
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v0.4 Pre-release
Pre-release
internal backplane

v0.3

18 May 17:18
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v0.3 Pre-release
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card lock slots

v0.2

18 May 17:18
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v0.2 Pre-release
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new attachment method

v0.1

18 May 17:19
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v0.1 Pre-release
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beginning stages of Oresat structural development

v0.5

18 May 17:18
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v0.5 Pre-release
Pre-release
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