Mikoyan Gurevich · Russia · ICAO: MiG19 · 1954–1968

The Mikoyan MiG-19 is the first most-produced supersonic aircraft powered by two jet engines capable of reaching supersonic speeds in level flight. It was a second-generation jet fighter developed by the Russian manufacturer, Mikoyan-Gurevich introduced in March 1955.

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Engine:
2× Tumansky RD-9B
Engine type:
Jet
Thrust:
2 × 7,100 lbf  ·  32 kN
Avionics:
RP-5 Izumrud radar, RWR, Basic <a href="https://aerocorner.com/blog/norden-bombsight/">bombsight</a>
Wing Tips:
No winglets
Seats:
1
Exterior length:
41 ft 0 in · 12.50 m
Tail height:
12 ft 10 in · 3.90 m
Fuselage diameter:
ft 3 in · 1.30 m
Wing span / rotor:
29 ft 6 in · 9.00 m
Max takeoff weight:
19,500 lb  ·  8,850 kg
Max Payload:
5,250 lb  ·  2,400 kg
Fuel capacity:
480 gal  ·  1,800 L  ·  1,500 kg  (Jet A)
Max cruise speed:
784 kt  ·  902 mph  ·  1,452 km/h
Range:
1,200 nm  ·  1,380 mi  ·  2,220 km
Ceiling:
57,400 ft  ·  17,500 m
Rate of climb:
35,000 ft/min  ·  178 m/s

Blog Mentions

Blog posts that mention the Mikoyan-Gurevich MiG-19:

10 Best Fighter Jets of the Vietnam War

In 1950, the manufacturing company Mikoyan-Gurevich started to develop a new fighter jet with a longer range compared to its predecessors Mig-15 and Mig-17 fighters. Powered by two Mikulin AM-5 axial jet engines, the designed aircraft could reach supersonic speeds in level flight.

On April 20, 1951, the Mikoyan-Gurevich Design Bureau was authorized to modify one of the prototypes and changed the Klimov VK-1 turbojet engine with two Mikulin AM-5s rated at 4,410 lbf each. In June 1955, the aircraft deliveries started.

The MiG-19s were sent to the Soviet Air Forces, and on July 3 of the same year, the aircraft was unveiled to the public in an airshow held at Tushino Airfield in Moscow.

Several variants of the MiG-19 were built. The MiG-19S is an upgraded single-crew day fighter designed with an all-movable slab tail and Svod long-range air navigation system receiver.

In 1956, the aircraft entered production. It has an external length of 12.54 meters with pitot probe retracted and 14.64 meters if extended, a height of 3.88 meters, and a fuselage diameter of 1.3 meters.

The wingspan is 9 meters, and the wing area is 25 square meters. Two Tumansky RD-9B afterburning turbojet engines powered the aircraft, with a dry thrust of 5,700 lbf each and 7,100 lbf with afterburner.

It has a gross weight of 7,560 kg, a maximum takeoff weight of 8,832 kg, and a fuel capacity of 480 gallons. The maximum speed at 33,000 feet is 784 knots.

It has a range of 750 nautical miles and a ferry range of 1,200 nautical miles with 200 gal drop tanks at 46,000 feet.

It can fly up to 57,400 feet and can climb at a rate of 35,000 feet per minute.

The MiG-19S is loaded with 3×30 mm Nudelman-Rikhter NR-30 autocannons, four hardpoints- two for drop fuel tanks and two for weapons, with a capacity of up to 500 kg of stores with provisions to carry combinations of two ORO-57K rocket pods and two FAB-250 general-purpose bombs.

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