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MiG-9 Technical Data
| Prime contractor: | Mikoyan-Gurevich Design Bureau |
| Country of origin: | Soviet Union |
| NATO codename: | Fargo |
| Function: | Fighter |
| Crew: | 1 |
| Year: | 1947 |
| Power plant: | Two RD-20F turbojets (copy of German BMW 003A engine) |
| Thrust: | 1,764 lb.each | 800 kg. each |
| Dimensions | | Wing span: | 32 ft.8 in. | 10.00 m. |
| Length: | 32 ft. 2 in. | 9.83 m. |
| Height: | 10 ft.6 in. | 3.22 m. |
| Weight: |
| Empty | 7,524 lb. | 3,420 kg. |
| Max. Takeoff | 11,119 lb. | 5,054 kg |
| Performance |
| Ceiling: | 44,280 ft. | 13,500 m. |
| Speed: | 566 mph. | 911 km/h. |
| Range: | 497 miles (w/max.payload)
683 miles (w/max.fuel) | 800 km. (w/max.payload)
1,100 km. (w/max.fuel) |
| Armament |
| One
N-37
37mm cannon with 40 rounds and two NS-23
23mm cannons with 80 rounds per gun. |
| Known Variants |
| MiG-9F, MiG-9FF MiG-9FR MiG-9FL MiG-9FS MiG-9UTI |
| Operators |
| Out of service |
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