Technical side of HEROS

Width 70 in 1,775 mm
Height 81.9 in 2,080 mm
Fuselage lenght 184 in 4,675.5 mm
Rotor diameter 165.75 in 4,210 mm
DOM 639 lbs 290 kg
Fuel capacity 30.1 US gal 114.2 litres
Maximum payload 440.9 lbs 200 kg
MAUW 1,234 lbs 560 kg
Cruising speed 75 kts 139 km/hr
Maximum speed 98 kts 181 km/hr
Maximum endurance 6 hours
Maximum hovering endurance 3.5 hours
Range 155 miles 250 km
Telemetry range 100 miles 160 km

Features

  •  HEROS has been developed as EASA EASA-CS27/EASA-CSVLR compliant
  •  A Category A twin-engine helicopter able to operate in 2nd performance class over congested areas
  •  Co-axial rotor – high effectivity, high stability, broad field of applications
  •  Long endurance (>4hours of flight)
  •  Ceiling >4000m MSA
  •  Professional design and projection
  •  Helicopter and cargo module interface
  •  In-flight and landing cameras
  •  Ballistic recovery parachute
  •  In-flight and cargo telemetry
  •  Transponder mode A, C, S
  •  Surface finish as per customer‘s wish
  •  Cargo module as per customer‘s specification
  •  Power – 2 piston engines ROTAX 503 (total output 100 hp)
  • Airframe – steel tube construction (L-CM3) with composite fuselage
  • Composite landing gear with dural skids
  • The UAV is equipped with camera system and IR searchlight
  • 12V el. system is powered with 2 generators (155W) and a backup 12 V battery.
  • Avionics
  • Sense and Avoid
  • IFPS – Inertial Flight Position System
  • DGPS – Differential GPS
  • Altimeter and airspeed indicator
  • LASER Altimeter
  • Radar/Ladar
  • PCU – Pilot Control Unit
  • Measuring aparature
  • The SSR Transponder
  • The UAV is BRS (ballistic recovery system) equipped