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MiG-3 Technical Data
| Prime contractor: | Mikoyan-Gurevich Design Bureau |
| Country of origin: | Soviet Union |
| Function: | Fighter |
| Crew: | 1 |
| Year: | 1941 |
| In-service year: | 1941 |
| Power plant: | One 1,350 hp. Mikulin AM-35A 12-cylinder liquid-cooled engine |
| Dimensions |
| Wing span: | 33 ft. 5 in. | 10.20 m. |
| Length: | 27 ft. 1 in. | 8.26 m. |
| Height: | 11 ft. 5 in. | 3.50 m. |
| Weight: |
| Empty | 5,938 lb. | 2,699 kg. |
| Max. takeoff | 7,370 lb. | 3,350 kg. |
| Performance |
| Ceiling: | 39,360 ft. | 12000 m. |
| Speed: | 398 mph. | 640 km/h. |
| Range: | 776 miles (w/max.fuel) | 1,250 km. (w/max.fuel) |
| Armament |
| One
UBS
12.7mm machine-gun, two ShKAS
7.62mm machine guns, later underwing pylons with two unsynchronised BS machine-guns added, FAB-25, FAB-50 or
FAB-100
bombs, underwing pylons for six RS-82 rockets, two chemical weapon containers. |
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