In numbers Through the lens Video
Technical specifications
| DESIGNER | OKB Yakovlev |
| COUNTRY | Russia |
| TYPE |
Fighter
|
| CREW | 1 |
| POWER-PLANT | One piston engine VK-105PD + Ligud-propellant rocket RD-1. |
| Power, h.p. | 1x1.240 |
| Thrust, kgf | - |
| DIMENSIONS | |
| Length, m | 8,50 |
| Height, m | 2,42 |
| Wing span, m | 9,20 |
| Wing area, m2 | 14,85 |
| WEIGHT | |
| Maximum take-off, kg | - |
| Normal take-off, kg | 2.980 |
| Empty aircraft, kg | 2.382 |
| Internal fuel, kg | - |
| Warload, kg | - |
| PERFORMANCE | |
| Maximum speed, km/h | 782 |
| Max speed in low height, km/h | 732 |
| Cruising speed, km/h | - |
| Range, km | - |
| Combat range, km | - |
| Service ceiling, m | 11.800 |
| Rate of climb, m/min | - |
| Maximum overload, g | - |
| ARMAMENT | One 23 mm cannon NS-23 with 60 rounds. |