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MiG-13 Technical Data
| Prime contractor: | Mikoyan-Gurevich Design Bureau |
| Country of origin: | Soviet Union |
| Function: | Fighter |
| Crew: | 1 |
| Year: | 1945 (I-250) |
| In-service year: | 1947 |
| Power plant: | One 1,650 hp. Klimov VK-107R 12-cylinder radial liquid-cooled engine and Khalshchevnikov VRDK booster |
| Dimensions |
| Wing span: | 31 ft. 2 in. | 9.50 m. |
| Length: | 26 ft. 9 in. | 8.19 m. |
| Height: | 10 ft. 1 in. | 3.08 m. |
| Weight: |
| Empty | 6,457 lb. | 2,935 kg. |
| Max. takeoff | 8,096 lb. | 3,680 kg. |
| Performance |
| Ceiling: | 39,000 ft. | 11,900 m. |
| Speed: | 513 mph. | 825 km/h. |
| Range: | 1,129 miles | 1,818 km. |
| Armament |
| One
VYa-23
23mm cannon and two
UBS
12.7mm machine guns, or three B-20
30mm machine guns |
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