VIT-2, N.N.Polikarpov

evelopment of the VIT-1 with new engines and yet more powerful armament. Twin tails provided better conditions for rear gunner;
First flown on May 11, 1938 by V.P.Chkalov, later by B.N.Kudrin (factory tests) and P.M.Stefanovskij (state acceptance tests). Performance was excellent. Decision was to launch series production with reduced armament, as a high speed dive bomber.
  • SPB - high speed dive bomber;
  • There was a project for long range unarmed version (7900km at 350km/h or 6200km at 500km/h) with M-105 engines. Not built.
  • "History of aircraft construction in the USSR" by V.B.Shavrov, Vol.2 p.21-22
    More links...
  • VIT-1/VIT-2 at Virtual Aircraft Museum
  • VIT-2, Polikarpov
  • Technical data
    Type VIT-2
    Function Multirole aircraft
    Year 1938
    Crew 3
    Engines 2*1050hp M-105
    Length 12.25m
    Wingspan 16.5m
    Wing area 40.76m2
    Empty weight 4032kg
    Loaded weight 6302kg
    Wing load 155kg/m2
    Power load 3.0kg/hp
    Speed (0m) 486km/h
    Speed (4500m) 513km/h
    Climb (5000m) 6.8min
    Ceiling 8200m
    Range 800km
    Takeoff Roll 22sec/450m
    Landing Roll 400m
    Guns 2*g37mm Sh (wing roots)
    2*g20mm ShVAK (wings)
    1*g20mm ShVAK (nose)
    1*g20mm ShVAK (turret)
    2*mg7.62mm ShKAS (ventral)
    Bombs 600kg (internal)
    2*500kg (external)
    Modified April 10, 1997
    by Alexandre Savine;
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