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Table 10 Modified Cessna 402 Cogeneration Architecture for high energy performances
Empty weight | Lb | 4,069 |
Useful load | Kg | 662 |
Max takeoff weight | Kg | 3107 |
Max on board fuel | Batteries (Boston Power Swing® 5300 Rechargeable Lithium-ion Cell) | |
Kg | 1050 | |
Wh/kg | 207 | |
Ah | 4,420 | |
Fuel | ||
Kg | 640 | |
Propulsion | ||
Cogen | Rolls Royce Model 250 | |
Power | kW | 250 |
Mass | Kg | 250 |
Motor | Four Plettemberg Nov. 150 mounted in two ACHEON Nozzle | |
Power | kW | 150 |
Mass | Kg | 11.5 |
Performances | ||
Max speed | m/s | 118.9 |
Max cruising speed | m/s | 109.4 |
Stall Speed | m/s | 46.3 |
Stall Speed Carriage | m/s | 25.1 |
Initial rate of climb | m/s | 7.366 |
Service ceiling | M | 8200 |
Long range cruising speed | m/s | 84.4 |
Range with reserves at economical cruising speed | km | 2000 |