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 (3,2 liters will last for 10 minutes flying in normal sport / scale aircraft)
- Fast spool times
- Three years warranty