Technical data
Type K-10
Function Trainer, Liaison, Agricultural
Year 1932
Crew 1
Engines 1*100hp M-11
Length 7.0m
Height 2.89m
Wingspan 10.7m
Wing area 18.0m2
Empty weight 700kg
Loaded weight 1035kg
Wing Load (kg/m2) 57.5
Power load (kg/hp) 10.4
Speed at 0m 175km/h
Cruise Speed 145km/h
Landing Speed 84km/h
Landing Roll 175m
Takeoff Roll 184m
Range 1200km
Flight Endurance 8.0h
Ceiling 3800m
1000m 7min
2000m 17min
3000m 34min
Fuel+Oil 190kg
Seats 1
Cargo ~100kg

K-10 by K.A.Kalinin

12k b/w "History of aircraft construction in the USSR", Vol.1 p.481

Two-seat low-wing monoplane with fixed landing gear. Wings were made folding for storage. Major roles:

Built in 1932, tested... and not entered series production.

  • "History of aircraft construction in the USSR", Vol.1 p.481;
  • ....

  • Created March 5, 1999 Back to
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