In numbers Through the lens Video
Three-view drawing
Technical specifications
| DESIGNER | OKB Nemana |
| COUNTRY | Russia |
| TYPE |
High-altitude reconnaissance aircraft
|
| CREW | 2 |
| POWER-PLANT | One piston engine M-25V |
| Power, h.p. | 1x730 |
| DIMENSIONS | |
| Length, m | 9,40 |
| Height, m | 3,80 |
| Wing span, m | 12,20 |
| Wing area, m2 | 26,80 |
| WEIGHT | |
| Maximum take-off, kg | - |
| Normal take-off, kg | 2.877 |
| Empty aircraft, kg | 2.197 |
| Internal fuel, kg | - |
| Warload, kg | - |
| - maximum | 400 |
| - standard configuration | 200 |
| PERFORMANCE | |
| Maximum speed, km/h | 370 |
| Max speed in low height, km/h | 340 |
| Cruising speed, km/h | - |
| Range, km | 1.300 |
| Combat range, km | - |
| Service ceiling, m | 6.700 |
| Rate of climb, m/min | 417 |
| Maximum overload, g | - |
| ARMAMENT | Two 7,62 mm machine-gun ShKAS with 450 rounds and one 7,62 mm machine-gun UBT with 600 rounds. |