In numbers Through the lens Video
Technical specifications
| DESIGNER | - |
| COUNTRY | Russia |
| TYPE |
Vertical, short take-off and landing
|
| CREW | - |
| POWER-PLANT | One or two turbojet engines |
| Thrust, kgf | 1x9.800 |
| DIMENSIONS | |
| Length, m |
10,81 / 7,0
|
| Height, m |
3,1 / 2,1
|
| Wing span, m |
4,0 / 4,0
|
| Wing area, m2 |
15,00
|
| WEIGHT | |
| Maximum take-off, kg | 7.400 |
| Normal take-off, kg | 6.100 |
| Empty aircraft, kg | 4.800 |
| Internal fuel, kg | 1.500 |
| Warload, kg | 1.100 |
| PERFORMANCE | |
| Maximum speed, km/h | 2.100 |
| Cruising speed, km/h | - |
| Service ceiling, m | 20.000 |
| Range, km | 2.200 |
| Combat range, km | 770 |
| Maximum overload, g | - |
| ARMAMENT |
Probably one or two 23mm guns. Transport of modern missiles.
|