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MiG-1 Technical Data
| Prime contractor: | Mikoyan-Gurevich Design Bureau |
| Country of origin: | Soviet Union |
| Function: | Fighter |
| Crew: | 1 |
| Year: | 1940 |
| In-service year: | 1940 |
| Power plant: | One 1,350 hp. Mikulin AM-35A 12-cylinder radial liquid-cooled engine |
| Dimensions |
| Wing span: | 33 ft. 5 in. | 10.20 m. |
| Length: | 26 ft. 8 in. | 8.16 m. |
| Height: | 8 ft. 6 in. | 2.62 m. |
| Weight: |
| Empty | 5,724 lb. | 2,602 kg. |
| Max. takeoff. | 6,818 lb. | 3,099 kg. |
| Performance |
| Ceiling: | 39,360 ft. | 12000 m. |
| Speed: | 389 mph. | 626 km/h. |
| Range: | 358 miles (w/max.payload) | 576 km/h. (w/max.payload) |
| Armament |
| One
UBS
12.7mm machine-gun, two ShKAS
7.62mm machine guns, later underwing pylons with two unsynchronised BS machine-guns added, two FAB-25, FAB-50 or
FAB-100
bombs, underwing pylons for six RS-82 rockets or two chemical weapon containers. |
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