DESIGN REQUIREMENTS

• Airworthiness requirements: according to FAR23
• Configuration: no restriction
• Powerplant: no restriction

Design features

• Low maintenance
• Low operating cost
• Flying controls: no restriction
• Structure: no restriction
• Landing gear: no restriction
• Power plant: no restriction
• Systems: no restriction
• Dimensions external: can be transported in a container (1m x 1.5m x 2m)

Payload

• Payload capacity: 2 kg excluding sensors and remote controls
• Payload volume: 0,3m x 0,3m x 0,3m

Performance:

• Takeoff: catapult launcher
• Landing: self landing, landing distance lower than 500 m on hard runway surface
• Top speed: 800 km/h.
• Stall speed: less than 140 km/h at the maximum weight
• Range: 150 km
• Endurance on site: 180 minutes (3h), Loiter speed: lower than 170 km/h
• Ceiling: no restriction
• Minimum turn radius: lower than 75 m