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- Mikoyan-Gurevich MiG-21
- Top speed: 2,175 km/h
- Wingspan: 7.15 m
- First flight: February 14, 1955
- Introduced: 1959
- Manufacturer: Mikoyan
- Engine type: Turbojet
Specifications (MiG-21-93)
General characteristics
- Crew: 1
- Length: 14.5 (with pitot) m (47 ft 6.86 in)
- Wingspan: 7.154 m (23 ft 5.66 in)
- Height: 4.125 m (13 ft 6.41 in)
- Wing area: 23.0 m2 (247.3 ft2)
- Gross weight: 8,825 kg (19,425 lb)
- Powerplant: 1 × Tumansky R25-300, 40.21 kN (9,040 lbf) thrust dry, 69.62 kN (15,650 lbf) with afterburner each
Performance
- Maximum speed: 2,175 km/h (1351.48 mph)
- Maximum speed: Mach 2.0
- Range: (internal fuel) 1,210 km (751 miles)
- Service ceiling: 17,800 m (58,400 ft)
- Rate of climb: 225 m/s (44,280 ft/min)
Armament
- 1x internal 23 mm GSh-23 cannon, plus
- 2x R-27R1 or R-27T or 4x Vympel R-77
- 2x 500 kg (1,102 lbs) bombs
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