| Technical data | |
|---|---|
| Type | Aktay |
| Function | Utility |
| Year | ? |
| Crew | 1 |
| Engines | 1*240hp rotary engine |
| Fuel consumption | 28 to 35kg/h |
| Length | ?m |
| Height | ?m |
| Rotor radius | ?m |
| Disc area | ?m2 |
| Empty weight | ?kg |
| Loaded weight | 1050kg |
| Power load (kg/hp) | 0.233 |
| Cruise Speed | 155km/h |
| Maximum Speed | 190km/h |
| Range (300kg cargo) |
100km |
| Range (190kg cargo) |
600km |
| Flight Endurance | 6h |
| Hovering Ceiling | 1300m |
| Service Ceiling | 4000m |
| Climb | |
| 1000m | ?min |
| Payload | |
| Fuel | ?kg |
| Seats | 2 |
| Cargo | 300kg |
Light multirole helicopter, created with traditional for Russian/Soviet products simplicity of maintenance, reliability under harsh conditions (snow, winder dust etc) and opportunity to use cheap automobile gasoline, oil and lubricants. Typical for Russia demands of reliable start under low temperatures also was met.
Keeping up with time, designers achieved low fuel consumption and noise levels. 'Aktay' features large luggage compartment and can accommodate stretcher and medical attendant for paramedic use.
| Predecessors | Modifications |
|---|---|
| ? | ? |
| References | Links |
|---|---|
|
|
| Created June 10, 1999 |
|
Back to Main Gate |