Technical data
Type I-230, 'D', MiG-3U
Function Fighter
Year 1942
Crew 1
Engines 1*1200/1350hp AM-35A
Length 8.62m
Wingspan 10.2m
Wing area 17.44m2
Empty weight 2627kg
Loaded weight 3260kg
Wing Load (kg/m2) 188
Power load (kg/hp) 2.4
Speed at 0m 526km/h
Speed at 7000m656km/h
Range 1300km
Ceiling 11900m
Climb to 5000m6.2min
Armament
Guns 2*20mm ShVAK

I-230, 'D', MiG-3U, A.I.Mikoyan/M.I.Gurevich


Development of the MiG-3, with the AM-35A engine. New wooden fuselage without central tube frame, cleaned water radiator, raised tailfin, oil cooler intakes in the wing roots, lighter landing gear, powerful cannon armament.

It was much closer to original N.N.Polikarpov 'Kh' project.

Performance was superior to one of the MiG-3. Series production was discussed, but was found unnecessary in 1943. Lavochkin and Yakovlev fighters production was increased, those aircraft fulfilled performance requirement.

Six were built, used on Kalinin front with a success.


PredecessorDevelopment

MiG-3
I-231

References:
  • "History of aircraft construction in the USSR", Vol.1 p.235-236;


  • More Links...
  • I-230, Mikoyan-Gurevich
  • I-230, Mikoyan-Gurevich

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