I-4bis by P.O.Sukhoj/A.N.Tupolev

15k b/w photo from the Virtual Aircraft Museum

M
onoplane variant of the I-4. Leading edge slats (half of the wing span) were controlled by the pilot. Engine cowling was replaced by Taunend ring with individual fairings over cylinder heads.
I-4bis was rebuilt from series I-4 for research purposes and flown in 1931. It was 10km/h faster than production aircraft, but suffered some losses in maneuverability. Other parameters remained unchanged. Slats proved to be helpful, but manual operation required too much attention from a pilot. It was found that slats should be made automatic... and the concept was abandoned until 1940.
PredecessorsModifications

I-4
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ReferencesLinks
  • "History of aircraft construction in the USSR" by V.B.Shavrov, Vol.1 p.367;
  • ....
  • Technical data
    Type I-4bis
    Function Experimental fighter
    Year 1931
    Crew 1
    Engines 1*480hp M-22
    Length 7.28m
    Wingspan 11.4m
    Wing area 19.8m2
    Empty weight 973kg
    Loaded weight 1385kg
    Wing load 70kg/m2
    Power load 2.88kg/hp
    Speed at 0m 268km/h
    Turn time 12sec
    Flight Endurance 2h18min
    Ceiling 7000m
    Climb
    1000m 14.0min
    Payload
    Fuel+Oil 236+25kg
    Armament
    Guns 2*mg7.62mm
    Created December 28, 1998
    by Alexandre Savine
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