Deviation Actions
Description
Photo taken at the McMinville Evergreen aviation and space museum in Northern Oregon. Photo taken by me, ask for permission to use.
The Mikoyan-Gurevich MiG-21 (Russian: Микоян и Гуревич МиГ-21; NATO reporting name: Fishbed) is a supersonic jet fighter and interceptor aircraft, designed by the Mikoyan-Gurevich Design Bureau in the Soviet Union. It was popularly nicknamed "balalaika", from the aircraft's planform-view resemblance to the Russian stringed musical instrument or ołówek (English: pencil) by Polish pilots due to the shape of its fuselage.
Early versions are considered second-generation jet fighters, while later versions are considered third-generation jet fighters. Approximately 60 countries over four continents have flown the MiG-21, and it still serves many nations six decades after its maiden flight. It made aviation records, became the most-produced supersonic jet aircraft in aviation history, the most-produced combat aircraft since the Korean War and previously the longest production run of a combat aircraft (now exceeded by both the McDonnell Douglas F-15 Eagle and General Dynamics F-16 Fighting Falcon).
National origin: Soviet Union
Design group: Mikoyan-Gurevich / Mikoyan
First flight: 14 February 1956 (Ye-2)
Introduction: 1959 (MiG-21F)
Status: In service (see list of operators)
Primary users: Soviet Air Forces (historical), Indian Air Force, Russian Air Force (historical)
Produced: 1959 (MiG-21F) – 1985 (MiG-21bis)
Number built: 11,496 (10,645 produced in the USSR, 657 in India, 194 in Czechoslovakia)
Variants: Chengdu J-7
General characteristics
- Crew: 1
- Length: 14.7 m (48 ft 2 in)
- Wingspan: 7.154 m (23 ft 6 in)
- Height: 4 m (13 ft 6 in)
- Wing area: 23 m² (247.6 ft²)
- Empty weight: 5,846 kg (12,880 lb)
- Loaded weight: 8,725 kg (19,230 lb) with 2 × K-13A missiles
- Max. takeoff weight: 9,800 kg (21,600 lb)
- Powerplant: 1 × Tumansky R-25-300 afterburning turbojet
- Dry thrust: 40.21 kN (9,040 lbf)
- Thrust with afterburner: 69.62 kN (15,650 lbf)
Performance
- Maximum speed:
- At sea level: Mach 1.05 (1,300 km/h; 808 mph)
- At 13,000 m (42,640 ft): Mach 1.76High altitude: Mach 1.8 (1,912 km/h, 1,032 knots) (2,175 km/h; 1,351 mph)
- Range: 1,470 km (910 mi; 790 nmi) at 10,000 m (32,800 ft) with 2 × K-13A missiles and 800 l (180 imp gal; 210 US gal)
- Service ceiling: 17,500 m (57,400 ft)
- Rate of climb: 225 m/s (44,280 ft/min)
- Wing loading: 452.2 kg/m² (92.7 lb/f²)
- Maximum g-load: 8.5 g
- Landing speed: 350 km/h (190 kn), usually with a drogue parachute
Armament
- Guns: 1 × internal 23 mm Gryazev-Shipunov GSh-23L autocannon with 200 rounds
- Hardpoints: 4 with a capacity of up to 2,000 kg (4,400 lb) of stores and provisions to carry combinations of: