SKELDAR V-200 Context

Specifications

  • Payload capacity: 40 kg
  • Max Speed Kmh: max airspeed 140 km/h
  • Endurance: 6+ h
  • Max Takeoff Weight: max takeoff weight 245 kg
  • Dimensions: Height 1.3 m; Width 1.2 m; Length 4 m
  • Features: Service ceiling 3,000 m; Rotor diameter 4.60 m
  • Power: Heavy fuel: Jet A-1, JP5 and JP8
  • Control Mode: High-level autonomous commands including Point and Fly and Point and Look
  • Range: Datalink range 100 km or more
  • System Role: VTOL tactical
  • Use Cases: Persistent ISR
  • Operating Environment: Authorised outdoor airspace

Comparable Systems

View SKELDAR V-200 overview