| Technical data | |
|---|---|
| Type | M-200 |
| Function | UTS |
| Year | ? |
| Crew | 2 |
| Engine | AI-25TL |
| Thrust | 2*1720kg |
| Length | 10.37m |
| Height | 4.20m |
| Wingspan | 9.40m |
| Wing area | ?m2 |
| Empty weight | 3805kg |
| Loaded weight | 4700kg |
| Wing Load (kg/m2) | ? |
| Thrust to Weight |
0.73 |
| Max. Speed at 0m | 850km/h |
| Cruise Speed | 700km/h |
| Takeoff Speed | 180km/h |
| Landing Speed | 155km/h |
| Landing Roll | 480m |
| Takeoff Roll | 200m |
| G-limits | +8/-3 |
| Ferry Range | 2200km |
| Operational Range | 1400km |
| Ceiling | 13100m |
| Climb | |
| 5000m | ?min |
| Payload | |
| Fuel | 1380kg |
| Armament | |
| Guns | ? |
| Bombs | ? |
| Rockets | ? |
Project of combat/trainer (UTS) twin-jet aircraft. Mid-wing conventional layout aircraft with trapezoidal wing of moderate sweep angle and aspect ratio. Depending on the training goal, programmable flight control system may be set to imitate behaviour of various civil and military aircraft in multitude of situations (flight regimes, failures etc). Active safety system is designed for this plane.
Variety of domestic (V.Ya.Klimov 35M) and foreign engines (1500...2000kg thrust each) may be fitted.
In combat situation M-200 may be modified to combat low-flying low-visibility targets like reconnaissance drones, cruise missiles or special strike aircraft.
As it is common today in Russia, project is not financed by The State.
| Predecessors | Modifications |
|---|---|
| n/a | n/a |
| References | Links |
|---|---|
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| Created October 18, 1999 |
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