| Technical data | ||
|---|---|---|
| Type | NV-2 | NV-2bis |
| Function | Trainer | |
| Year | 1935 | 1938 |
| Crew | 1 | 1 |
| Engine | 100hp M-11 | 165hp MG-11. |
| Length | 6.15m | |
| Wingspan | 8.0m | |
| Wing area | 11.0m2 | |
| Empty weight | 385kg | 435kg |
| Loaded weight | 750kg | 800kg |
| Wing Load (kg/m2) | 68.0 | 72.7 |
| Power load (kg/hp) | 7.50 | 4.85 |
| Speed at 0m | 230km/h | 260km/h |
| Landing Speed | 75km/h | |
| Flight Endurance | 10hmin | 7hmin |
| Ceiling | 5800m | 7000m |
| Payload | ||
| Fuel+Oil | 250+25kg | |
NV-2 and NV-2bis by V.V.Nikitin
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Single-seat low-wing monoplane trainer, with 100hp M-11 engine in NACA cowling. Fuselage and wing - of plywood design, covered with fabric. Main landing gear was retractable backwards into underwing fairings.
NV-2 was built in 1935 at Moscow Aviation High School (Aviatechnicum) on Osoaviakhim money. Flight test were passed easily, flight performance was superior.
More than 150 flights were performed on the NV-2.
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In 1938 OKB-30 released the second aircraft of the NV-2 family, the NV-2bis. It was powered by 165hp MG-11. Aircraft passed all trials and VVS ordered small series of 10 planes. Construction started, but terminated when production of the UT-2 was ordered on the same factory.
| Predecessors | Modifications |
|---|---|
| None |
 NV-2bis-MG-31 UTI-5 |
| References | Links |
|---|---|
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