Designing EagleSat’s Structure

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Presentation transcript:

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

Revision 2 - Rails

Revision 2 – Cross Spar/Bracket

Revision 2 - Complete

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

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

Revision 3 - Rails

Revision 3

Revision 3 - Brackets

Revision 3 – Pumpkin OBC Compatibility

Revision 3 - Complete

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

Thank you for listening