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