 |
 |
 |
 |
|
 |
|
 |
 |
|
|
|
|
 |
|
 |
|
 |
|
 |
 |
 |
 |
 |
 |
 |
 |
|
 |
|
 |
|
|
|
 |
|
 |
Vertical Take Off and Landing
aircraft "KARLSSON"
Specifications
| Dimensions External: |
Dimensions Internal: |
| Wingspan | 6,8m; 22,3 ft |
Cabin Lenght | 1,43m; 4,7 ft |
| Lenght | 6,1m; 20 ft |
Cabin width | 1,3m; 4,26 ft |
| Height overall | 2,51m; 8,2 ft |
Cabin height | 1,25m; 4,1 ft |
|
|
| Power Plant: |
Weights |
| Two Piston Engines | 200 HP each | Max VTOL weight | 650kg; 1430lb |
| Engine Type | 4 cylinder | STOL weight | 720kg; 1630lb |
| Transmission | Mechanical |
|
|
| Performans, Standart Day: |
| Max Speed | 510km/h; 310 mph |
| Service Ceiling | 5,500m; 18,000 ft |
| Hovering Ceiling | 1,200m; 3,950 ft |
| Range, VTOL, no reserves | 1,100km; 685miles |
| Range, STOL, no reserves | 2,100km; 1,300miles |
| Safety Measures: |
| All three fans are mechanically interconnected. All transmission gearboxes are constantly monitored by heat and oil chip gauges. Aircraft can continue horizontal flight with one engine failure. Aircraft can land as conventional airplane.
|
|
|
 |
 |
 |
|
 |
|
 |
|
 |
|
 |
|
 |
|
 |
|
 |
|
 |
|
 |
|
 |
|
 |
|
 |
|
|
 |
|
 |
|
|
|
|
 |
|
|
|
|
|
 |
|
|
 |
 |
|
 |
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|