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MiG-5 Technical Data
| Prime contractor: | Mikoyan-Gurevich Design Bureau |
| Country of origin: | Soviet Union |
| Function: | Long range escort fighter |
| Crew: | 1 |
| Year: | 1941 ("T"-version) 1942 ("IT"-version) |
| In-service year: | 1941 |
| Power plant: | Two 1,700 hp. each Shvetsov M-82F 12-cylinder radial liquid-cooled engines ("IT" version) |
| Dimensions |
| Wing span: | 49 ft. 5 in. | 15.10 m. |
| Length: | 38 ft. 9 in. | 11.85 m. |
| Height: | 11 ft. 2 in. | 3.40 m. |
| Weight: |
| Empty | 16,731 lb. | 7,605 kg. |
| Max. takeoff | 17,600 lb. | 8,000 kg. |
| Performance |
| Ceiling: | 32,144 ft. | 9,800 m. |
| Speed: | 375 mph. | 604 km/h. |
| Range: | 1,553 miles | 2,500 km. |
| Armament |
| One
VYa-23
23mm cannon, two BS
12.7mm machine-guns , four ShKAS
7.62mm machine-guns |
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