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Designing EagleSat’s Structure

Designing EagleSat’s Structure. Aaron Taylor Space Grant Intern. Overview. Cube Satellite Requirements Revision 1 Revision 2 Revision 3 Future Work. Requirements. Revision 1. Revision 2 Goals. Reduce amount of material used Quick assembly/disassembly for easy board access.

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Designing EagleSat’s Structure

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  1. Designing EagleSat’s Structure Aaron Taylor Space Grant Intern

  2. Overview • Cube Satellite Requirements • Revision 1 • Revision 2 • Revision 3 • Future Work

  3. Requirements

  4. Revision 1

  5. Revision 2 Goals • Reduce amount of material used • Quick assembly/disassembly for easy board access

  6. Revision 2 - Rails

  7. Revision 2 – Cross Spar/Bracket

  8. Revision 2 - Complete

  9. Revision 2 - Challenges • Difficult to assemble • All screws required a nut • Bracket system was inefficient

  10. Revision 3 - Goals • Make all screws mount externally • Simplify the brackets • Make the structure Pumpkin OBC compatible

  11. Revision 3 - Rails

  12. Revision 3

  13. Revision 3 - Brackets

  14. Revision 3 – Pumpkin OBC Compatibility

  15. Revision 3 - Complete

  16. Future Plans • FEM Analysis • Thermal and vibration testing • Make necessary revisions based on lab and Balloon flight testing.

  17. Thank you for listening

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