The Mikoyan MiG-29 Fulcrum
Is a fourth-generation jet fighter
aircraft designed in the Soviet Union for an air superiority role.
Developed in the 1970s by the Mikoyan design bureau,
it entered service with the Soviet Air Force in
1983, and remains in use by the Russian Air
Force as well as in many other nations. The NATO name
"Fulcrum" was sometimes unofficially used by Soviet pilots in
service.
Specifications (MiG-29)
General characteristics
Crew: 1
Length: 17.37 m (57 ft)
Wingspan: 11.4 m (37 ft 3 in)
Height: 4.73 m (15 ft 6
in)
Wing area: 38 m² (409 ft²)
Empty weight: 11,000 kg
(24,250 lb)
Loaded weight: 15,300 kg
(33,730 lb)
Max. takeoff weight: 20,000 kg
(44,100 lb)
Powerplant: 2 × Klimov RD-33 afterburning turbofans, 8,300 kgf (81.4 kN, 18,300 lbf) each
Performance
Maximum speed: Mach 2.25 (2,400 km/h, 1,490 mph) At low
altitude: Mach 1.25 (1,500 km/h, 930 mph)
Range: 1,430 km (772 nmi, 888 mi) with maximum
internal fuel
Ferry range: 2,100 km (1,300 mi) with 1 drop
tank
Service ceiling: 18,013 m (59,100
ft)
Rate of climb: initial 330 m/s
average 109 m/s 0–6000 m(65,000 ft/min)
Wing loading: 442 kg/m²
(90.5 lb/ft²)
Thrust/weight: 1.08
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