Design Features

Mechanical

  • Twin Thrust Vectoring Motors
  • Carbon Fiber Clam Shell Construction
  • Single Operation Latch
  • Isolated Electronics Enclosure
  • Hinge on Leading Edge to Acces Payload from Rear
  • Wing Span of ~2m

Electrical

  • 200 W Solar Cell Array
  • BMS With Battery Cell Balancing
  • Maximum Power Point Tracking Solar Charging Loop
  • Redundant IMU
  • Custom 6S4P Battery Pack Using 18650 Cells

Software

  • Separate Hover and Fixed Wing Flight Modes
  • Closed Loop Roll/Pitch/Yaw Stabilization
  • Closed Loop Altitude Control
  • Ground Station Software to Plan Missions
  • GPS Way Point Tracking

Specifications

  • 100 Km Range @ 150 KPH
  • 400 Km Range @ 60 KPH
  • Unlimited Range With Landing for Solar Recharge
  • 2 Kg Max Payload
  • Insulated Payload For Temperature Sensitive Goods
  • Two 40x80 cm Cargo Bays
  • Autonomous Take Off, Cruising, and Landing
  • Self-Charging Using Solar Panel
  • Wireless Mission Programming

Our latest flight shows over a minute of stable flight