| Technical data |
| Type |
U-2 (SP) |
| Function |
Liaison |
| Year |
1933
|
| Crew |
1 |
| Engines |
1*100hp M-11
|
| Length |
8.1m |
| Height |
?m |
| Wingspan |
11.4m |
| Wing area |
33.1m2 |
| Empty weight |
662kg |
| Loaded weight |
1000kg |
| Wing Load (kg/m2) |
30.2 |
| Power load (kg/hp) |
10.0 |
| Maximum Speed |
148km/h |
| Landing Speed |
67km/h |
| Landing Roll |
100m |
| Takeoff Roll |
140m |
| Range |
550km |
| Flight Endurance |
4h |
| Ceiling |
3300m |
| Climb |
| 1000m |
9min |
| 2000m |
22min |
| 3000m |
40min |
| Payload |
| Fuel+Oil |
90+12kg |
| Seats |
2 |
| Cargo |
(some)kg |
U-2SP, SP, U-2 Special Purpose by N.N.Polikarpov
Modification of U-2 Aeropyl (duster) for local liaison, passenger and cargo transportations. Tank and dispenser were replaced by two single-seat cockpits. Controls - only in pilot's cockpit. This variant was built in large numbers. 861 rolled out during 1934- 1939 period.
| Predecessors |
Modifications |
U-2(AP)
|
? |
