190R Donneés techniques

Technical spec.

Hawk 190R technical figures
Every engine is delivered with its own unique performance data sheet.

 

Example of typical data:
Thrust range 0.5 – 19.0 kg  / 1.3 – 41.9  lbs    +/- 5%
Pressure ratio 1.2 – 3.9
Rpm 39 000 – 130 000 rpm
EGT 390 – 760° (max 800) Celsius
Fuel consumption 50 – 390g / minute
Fuel Kerosene, Jet A1 or Diesel (EN590) with 1.5% oil
Oil quality Two-stroke outboard oil
Engine controll Fadec full auto start
Starting gas Propane butane mixture
Battery LiPo 7.4, 2000mAh (Not incl.)
Mounting Lugs with fuel / propane connectors
Compressor Radial, transonic in-house design
Turbine Radial
Combustor Reverse flow type
Engine weight 2800 gram (engine and starter)
Airborne Install weight Aprox. 3100 gram

All data in ISA conditions.

 

Unique features for the Hawk 190R

  • Unique rotor damping system
  • Milled in house designed compressor
  • Mounting lugs of solid aluminium with fuel connectors
  • Lowest fuel consumption on the market (3,2 liters will last for 10 minutes flying in normal sport / scale aircraft)
  • Fast spool times
  • Three years warranty