Fixed Wing 2025

Fixed Wing 2025

Initial Planning

  • Name

    • Eclipse

  • High Level Specs

    • 1.5 m wingspan

    • Max takeoff weight = 5kg

    • 6S Battery Voltage

      • ~1.1kg of batteries

      • one 6S battery pack only

      • battery chemistry options: Li-ion, Li-Po, LiHv

    • Modular wings & fuselage

  • Purpose, Quantity, & Timeline

    • High Level

      • Pursue the primary purpose for roughly a full year with this plane and then hand it off to other subteams for learning in the secondary purpose before decommissioning

    • Quantity

      • A single aircraft will be built (and maintained in the unlikely event of damage)

    • Primary purpose

      • learning how to design fixed wings → mechanical skills

      • learning how to operate fixed wings → ardupilot & pilot skills

    • Secondary purposes

      • Custom battery long term? Could be saved for VTOL depending on EE interest​

      • flight testing bench for EE and EFS new CAN architecture. ​

      • testing EFS milestones milestones​ M2 and M3

      • testing EE ZP3 hardware designs

  • Budgeting

    • Will be less expensive than fancy composites

    • Will be more expensive than hacked together foam planes we’ve done in the past

Related Resources

Mechanical

All mechanical design documents can be found in Eclipse Mechanical Decisions Documentation.

more mechanical information is currently stored in Eclipse 2025 .

Electrical

Electrical Components

Electronics System Diagram

Electronics Harness Diagrams

Eclipse Harness.pdf · UWARG/hardware · GitHub

Electronics Placement Diagram

 

FF51EF34-AA44-44C4-B9F2-8F84B4C6C337-20240824-181836.jpeg

 

Maiden Flight Electronics System Diagram

 

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