An Open Access Journal
Geometric data | ||||||||
Wing span | m | 13.45 | Ft | 44.2 | ||||
Length | m | 11.09 | Ft | 36.5 | ||||
Height | m | 3.49 | Ft | 11.6 | ||||
Wing Area | m2 | 21 | Sq ft | 225.8 | ||||
Aerodynamic constants | ||||||||
CD | – | 0.026 |  |  | ||||
E | – | 0.85 |  |  | ||||
CLmax | – | 2.27 |  |  | ||||
Weights | ||||||||
Empty weight | kg | 1845 | Lb | 4,069 | ||||
Useful load | kg | 1262 | Lb | 2,783 | kg | 662 | lb | 1459.46 |
Max takeoff weight | kg | 3107 | Lb | 6,850 | ||||
Max on board fuel | kg | 640 | Gal | 213 | Batteries (Boston Power Swing® 5300 Rechargeable Lithium-ion Cell) | |||
kg | 1550 | |||||||
Wh/kg | 170 | |||||||
Ah | 4,420 | |||||||
Propulsion | ||||||||
Engine | Two 240Â kW (325Â hp) turbocharged and fuel injected TSIO-520-VBs | Four Plettemberg Nov. 15 mounted in two ACHEON Nozzle | ||||||
Power | kW | 240 | Hp | 325 | kW | 150 | hp | 203 |
Weght | kg | 219.5 | Lb | 484 | kg | 11.5 | lb | 25.4 |
Performances | ||||||||
Max speed | m/s | 118.9 | Kts | 230 | ||||
Max cruising speed | m/s | 109.4 | Kts | 213 | ||||
Stall Speed | m/s | 46.3 | Kts | 71.4 | ||||
Stall Speed Carrriage | m/s | 25.1 | Kts | 48.9 | ||||
Initial rate of climb | m/s | 7.366 | ft/min | 1,450 | ||||
Service ceiling | m | 8200 | Ft | 26,900 | ||||
Long range cruising speed | m/s | 84.4 | Kts | 164 | To be calculated | |||
Range with reserves at economical cruising speed | km | 2360 | Nm | 1273 | To be calculated |