FABE Industrial Latina de Aeronaves – Meet the SKT UAS-OPH Helicopter

Specifications

Fuslage Diameter (LWH): 6.57m x 1.3m x 1.8m
Diamter Rotor: 7m
Diameter Tail Rotor: 1.4m
Landing Gear (L*W): 1.8m x 1.92m
Empty Weight: 350kg
MTOW: 700kg
Payload: 350kg
Cruising Speed: 90kts (166km/h)
Max. Speed: 110kts (204km/h)
Engine: Piston
Fuel: Gasolin/MoGas
Standart Tank: 148L
Consumption: 25L/h (18.75kg)
Operation Altitude: 10.000ft / 3.048m
Ceiling Altitude: 15.000ft / 4.572m
LOS Range: 200km (Radius)
BLOS (SATCOM): 1’000+km
MIMO/MESH: Depending Relais
Stations
Noise Level (dB): 77 dB
Payload/MTOW Rate: 50%
Manned/Unmanned: OPH

Endurance/Payload

  • Consumption 25L/h = 18.75kg
  • Standart Tank 148L = 111kg = Endurance 5.92/h
  • Plus net Payload 239kg (Example)
  • Endurance per hour +18.75kg Fuel – Total Payload 350kg

SKT UAS-OPH Ultra Light Engine

  • 4-stroke, 6-cylinder, 3.9L, boxer engine with side valve (flat head)
  • Multi-point fuel injection, Turbocharged
  • Electronic ignition
  • Liquid cooling
  • Highest quality standards for crankshafts, connecting rods, camshafts and all engine parts
  • FADEC (Full Authority Digital Engine Control) comprising an unique 3 ECU Control Systems for improved redundancy & safety.
  • European design & manufactured
  • Airworthiness approval: LAS for USA and DULF for Germany

Performance

  • Lightweigth: Installed dry weight (liquids 7kg): 92kg
  • Silent engines (2.800 RPM)
  • Gasoline / MoGas driven
  • Power: Max. power 170hp – Continuous power 150hp,nearly flat torque diagram (always the power you need)
  • Compact (LxWxH): 649x 466 x 555 mm
  • TBO: 1’800 hrs