| General Information |
| Type |
NV-4
|
| Function |
Amphibian |
| Year |
1936
|
| Crew |
2 |
| Powerplant |
| Type |
MG-11
|
| Power |
100hp |
| Size |
| Length |
8.7m |
| Height |
?m |
| Wingspan |
10.5m |
| Wing area |
28.5m2 |
| Weights and loads |
| Empty |
825kg |
| Loaded |
1090kg |
| Wing Load (kg/m2) |
38.2 |
| Power load (kg/hp) |
10.9 |
| Speed |
| at 0m |
160km/h |
| Landing |
65km/h |
| Roll |
| Landing |
?m |
| Takeoff |
?m |
| Range |
| Practical |
?km |
| Flight Endurance |
?h |
| Ceiling |
| Ceiling |
?m |
| Climb |
| 1000m |
?min |
| Payload |
| Fuel+Oil |
90+15kg |
Two-seater biplane amphibian. Aircraft of all-wooden construction with one large float and pair of underwing balance floats. Upper wing carried ailerons, the lower one - landing flaps. Grumman-type landing gear was retracted manually. NV-4 was equipped for blind flight.
Aircraft was built in 1936 in Moscow and flown. But V.V.Nikitin was assigned to other projects and could not to supervise trials program.
NV-4 was abandoned.
| Predecessors |
Modifications |
| - |
- |
