K-10 by K.A.Kalinin

wo-seat low-wing monoplane with fixed landing gear. Wings were made folding for storage. Major roles:
  • trainer with dual controls;
  • liaison;
  • agricultural 'duster';
    Built in 1932, tested... and not entered series production.
  • "History of aircraft construction in the USSR" by V.B.Shavrov, Vol.1 p.481;
  • ....
  • 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 57.5kg/m2
    Power load 10.4kg/hp
    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
    Created March 5, 1999
    by Alexandre Savine
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