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MiG-8 Technical Data
| Prime contractor: | Mikoyan-Gurevich Design Bureau |
| Country of origin: | Soviet Union |
| Function: | Experimental airplane |
| Crew: | 1+2 passengers |
| Year: | 1945 |
| Power plant: | One 110 hp. M-11VM 5-cylinder air-cooled engine |
| Dimensions |
| Wing span: | 31 ft. 2 in. | 9.5 m. |
| Length | 23 ft. | 7 m. |
| Height: | 8 ft. 2 in. | 2.5 m. |
| Weight: |
| Empty | 1,408 lb. | 640 kg. |
| Max. takeoff | 2,530 lb. | 1,150 kg. |
| Performance |
| Ceiling: | 17,056 ft. | 5,200 m. |
| Speed: | 127 mph. | 205 km/h. |
| Range: | 310 miles | 500 km. |
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