Puma
Design
Gallery
Statistic test
Technical data: | |
Wingspan | 9,15m |
Length | 6,27m |
Height | 2,30m |
Cabin width | 1,24m |
Wing area | 11,3m2 |
Wing root airfoil | NACA 4415 |
Wing tip airfoil | NACA 4412 |
Wing torsion | -2,4 stopnia |
Horizontal tail area | 2,1m2 |
Vertical tail area | 1m2 |
Airfoil | NACA0012 |
Weight and Performance: | |
Empty Weight | 290kg |
Max. Takeoff Weight | 472,5 kg |
Payload | 182,5 kg |
Max Fuel Capacity | 2x50 l |
Max. Load Factors | +4 / -2 |
Stall Speed (without flaps) | 77 km/h |
Stall Speed (with flaps) | 61 km/h |
Cruising Speed | 220 km/h |
Never Exceed Speed | 270 km/h |
Max. Speed in horizontal flight | 240 km/h |
Rate of climb | 8 m/s |
Ceiling | 3650 m |
Range (45min. reserves) | 1200 km |