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

33k b/w from "History of aircraft construction in the USSR", Vol.1 p.476

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.

PredecessorsModifications

U-2(AP)
?

ReferencesLinks
  • "History of aircraft construction in the USSR", Vol.1 p.477;
  • ....

  • Created June 18, 1999 Back to
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