Motore - Reggiane fighters
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Main menu:
Aircraft > RE2006
ENGINE
The engine was a 12 cylinders V water cooled engine run by gasoline direct injection and produced by Daimler Benz.
Technical features:
Power at altitude, climb&combat | 1510 HP @ 5700 m |
Power at 0 m, takeoff | 1750 HP |
| Nr. of cylinders | 12 |
Displacement | 44510 cc |
Bore | 162 mm |
Stroke | 180 mm |
Fuel supply system | Bosch direct injection |
Ignition system | Bosch |
| Compressor | Centrifugal, hydraulic |
Injectors per cylinder | 1 |
Spark plugs per cylinder | 2 |
Valves per cylinder | 4 |
Compression ratio | 7.5/7.3:1 |
Dry weight | 890 kg |
Performance chart
Running conditions allowed:
Altitude [km] | Condition | Engine speed [rpm] | Power [HP] | Intake pressure [kg/cm2] |
| 0 | Takeoff and emergency | 2700 | 1750 | 1.40 |
| 0 | Climb and combat | 2500 | 1580 | 1.30 |
| 0 | Max continuous power | 2300 | 1375 | 1.20 |
| 5.7 | Emergency | 2700 | 1620 | 1.40 |
| 5.7 | Climb and combat | 2500 | 1510 | 1.30 |
5.4 | Max continuous power | 2300 | 1400 | 1.20 |
| 5.0 | Low consumption max continous power | 2000 | 1170 | 1.05 |
