Time Period: Post-WW2
Country of Origin: Russia & USSR
Type: Fighter Aircraft
Manufacturer: Mikoyan-Gurevich
Mikoyan-Gurevich MiG-21 Aircraft Overview
The Mikoyan-Gurevich MiG-21 is a supersonic fighter aircraft that was developed by the Soviet Union in the late 1950s and early 1960s. It was one of the most widely used fighter jets of the Cold War era and saw service with many countries around the world.
The MiG-21 was designed by the Mikoyan-Gurevich design bureau, which was headed by Artem Mikoyan and Mikhail Gurevich. The aircraft first flew in 1956 and entered service with the Soviet Air Force in 1959. The MiG-21 was powered by a single Tumansky R-25 turbojet engine, which gave it a top speed of over Mach 2 and a range of over 1,000 miles.
The MiG-21 was armed with a variety of weapons, including air-to-air missiles, unguided rockets, and bombs for ground attack missions. It was known for its agility and high rate of climb, which made it a formidable opponent in air-to-air combat. The aircraft was also relatively inexpensive to produce and maintain, which made it attractive to many countries looking to acquire modern fighter aircraft.
The MiG-21 saw extensive combat during the Vietnam War, where it was used by the North Vietnamese Air Force against United States forces. It also saw service in many other conflicts around the world, including the Arab-Israeli Wars, the Iran-Iraq War, and the India-Pakistan Wars. The MiG-21 remains in service with many countries to this day, although it has largely been replaced by newer aircraft such as the MiG-29 and Su-27.
Mikoyan-Gurevich MiG-21bis Specifications
- Crew: 1
- Length: 14.7 m (48 ft 3 in) excluding pitot boom
- Wingspan: 7.154 m (23 ft 6 in)
- Height: 4.1 m (13 ft 5 in)
- Wing area: 23 m2 (250 sq ft)
- Airfoil: root: TsAGI S-12 (4.2%); tip: TsAGI S-12 (5%)
- Gross weight: 8,725 kg (19,235 lb) with two R-3S missiles
- Max takeoff weight: 8,800 kg (19,401 lb) unprepared or metal planking runway. 9,800 kg (21,605 lb) paved runway with standard wheels and tyres. 10,400 kg (22,928 lb) paved runway with larger wheels and tyres
- Powerplant: 1 × Tumansky R-25-300 afterburning turbojet, 40.18 kN (9,030 lbf) thrust dry, 69.58 kN (15,640 lbf) with afterburner
Mikoyan-Gurevich MiG-21bis Performance
- Maximum speed: 2,175 km/h (1,351 mph, 1,174 kn) / M2.05 at 13,000 m (43,000 ft). 1,300 km/h (810 mph; 700 kn) / M1.06 at sea level
- Landing speed: 250 km/h (160 mph; 130 kn)
- Range: 660 km (410 mi, 360 nmi) clean at 11,000 m (36,089 ft). 604 km (375 mi; 326 nmi) at 11,000 m (36,089 ft) with two R-3S missiles. 793 km (493 mi; 428 nmi) at 10,000 m (32,808 ft) with two R-3S missiles and 800 L (210 US gal; 180 imp gal) drop-tank
- Service ceiling: 17,500 m (57,400 ft)
- Time to altitude: 17,000 m (55,774 ft) in 8 minutes 30 seconds
- Thrust/weight: 0.76
- Take-off run: 830 m (2,723 ft)
- Landing run with SPS and brake parachute: 550 m (1,804 ft)
Mikoyan-Gurevich MiG-21bis Armament
- Guns: 1 × internal 23 mm Gryazev-Shipunov GSh-23L autocannon with 200 rounds
- Hardpoints: 5 (4 underwing + 1 ventral, reserved for fuel droptanks) , with provisions to carry combinations of:
- Rockets: 4 × S-24 or 4× UB-16-57 rocket pods (4×16 57mm rockets)
- Missiles: ;* Air-to-air missiles:
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- K-13
- R-55
- R-60
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- Bombs: 2 × 500 kg (1,100 lb) and 2 × 250 kg bombs