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Hawk 240R Technical spec. Fuel Figures Performance Dimensions
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Technical spec.

Hawk 240R technical figures

 

Every engine is delivered with its own unique performance data sheet.

 

Example of typical data:

 

Thrust range                                       0.8 - 24.0 kg  / 1.8 - 52,9  lbs    +/- 5%

 

Pressure ratio                                      1.2 - 4,6

 

Rpm                                                   39 000 - 132 000 rpm

 

EGT                                                   400 - 760° ( max 800) Celsius

 

Fuel consumption                                 65 - 515g / 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 240R

  • Unique rotor damping system
  • Milled in house designed compressor
  • Mounting lugs of solid aluminium with fuel connectors
  • Lowest fuel consumption on the market (4,5 liters will last for 10 minutes flying in normal sport / scale aircraft)
  • Fast spool times
  • Three years warranty