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MiG-9 Fargo

MiG-9 Fargo Specification
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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