Technical data
Type I-301T
Function Trainer, Experimental
Year 1946
Crew 2
Engines 2*800kg RD-20
Length 9.83m
Wingspan 10.0m
Wing area 18.2m2
Empty weight 3584kg
Loaded weight 4812kg
Wing Load (kg/m2) 264
Power load (kg/hp) 3.01kg/kgf
Maximum Speed 900km/h
Landing Speed 190km/h
Turn time 37sec
Range 530km
Ceiling 12500m
5000m 5.0min
Guns 1*g37mm NS-37
2*g23mm NS-23

I-301/FT, A.I.Mikoyan/M.I.Gurevich

11k FT-1 - eject!8k drawing of the FT-2
"History of aircraft construction in the USSR", Vol.1 p.306

The I-301T (FT) was a two-seat trainer development of the MiG-9.

Two built (FT-1 and FT-2), slightly differing by canopy shape. Used for pilot training and for experiments with ejectable seat (from the rear cockpit). It was the first Soviet aircraft to be equipped with ejectable pilot seat.

  • "History of aircraft construction in the USSR", Vol.1 p.305-308;

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  • I-301, Mikoyan-Gurevich

  • Modified October 23, 1997 Back to
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