Technical specifications 
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THREE-VIEW DRAWING
TECHNICAL SPECIFICATIONS
| DESIGNER | OKB Nemana |
| COUNTRY | Russia |
| TYPE | High-altitude Reconnaissance aircraft |
| CREW | 2 |
| POWER-PLANT | One reciprocating motor M-25 V |
| Thrust, h.p | 1 x 730 |
| DIMENSIONS | |
| Length, m | 9,40 |
| Height, m | 3,80 |
| Wing span, m | 12,20 |
| Wing area, m2 | 26,80 |
| WEIGHT | |
| Normal take-off, kg | 2.877 |
| Empty aircraft, kg | 2.197 |
| Maximum take-off, kg | - |
| Internal fuel, kg | - |
| PERFORMANCE | |
| Maximum speed, km/h | 370 |
| Cruising speed, km/h | - |
| Max speed in low height, km/h | 340 |
| Rate of climb, m/min | 417 |
| Service ceiling, m | 6.700 |
| Range, km | 1.300 |
| Combat range, km | - |
| ARMAMENT | Two 7,62 mm machine-gun ShKAS (450 rounds) and one 7,62 mm machine-gun UBT (600 rounds). Warload-max 400 kg. |
