| 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 |
| Climb | |
| 5000m | 5.0min |
| Armament | |
| Guns | 1*g37mm NS-37
2*g23mm NS-23 |
I-301/FT, A.I.Mikoyan/M.I.Gurevich
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|
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| 11k FT-1 - eject! | 8k drawing of the FT-2 |
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.
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