Credit
Gojanovic123456789 · CC BY-SA 4.0 · Resized · CC BY-SA 4.0 · Source ↗ · Modified
FORCETALLY
Loading the evidence…
Preparing your view.
Preparing your view.
At a glance
Measured figures
MiG-21bis · excluding pitot boom
Single source14.7 m (48 ft 3 in) excluding pitot boom[source]
Length
Single sourceConfiguration
| Specification | Mikoyan-Gurevich MiG-21 | Sukhoi Su-33 |
|---|---|---|
| Type | Fighter and interceptor aircraft[source] | Carrier-based air superiority fighter with multirole capabilities[source] |
| National origin | Soviet Union[source] | Soviet Union Russia[source] |
| Designer | Mikoyan-Gurevich[source] | — |
| Status | In service[source] | In service[source] |
21.19 m (69 ft 6 in)[source]
wing folded
Single source7.40 m (24 ft 3 in) wing folded[source]
Gross; MiG-21bis · with two R-3S missiles
Single sourceMaximum take-off; MiG-21bis · unprepared or metal planking runway
Single source8,725 kg (19,235 lb) with two R-3S missiles[source]
8,800 kg (19,401 lb) unprepared or metal planking runway[source]
Empty; Empty weight
Single sourceGross; Gross weight
Single sourceMiG-21bis · 1 × Tumansky R-25-300 afterburning turbojet thrust dry
Single sourceMiG-21bis · with afterburner
Single source1 × Tumansky R-25-300 afterburning turbojet, 40.18 kN (9,030 lbf) thrust dry, 69.58 kN (15,640 lbf) with afterburner[source]
2 × Saturn AL-31F3 afterburning turbofan engines thrust each dry
Single sourcewith afterburner
Single source48,400 ft/min
Single source246 m/s (48,400 ft/min)[source]
Bars compare reported quantities only. A larger figure does not make a system better; configurations and test conditions differ.
| Primary users |
|---|
Soviet Air Forces (historical) Indian Air Force (historical) North Korean Air Force Angolan Air Force[source] |
| — |
| Number built | 11,496 (10,645 produced in the USSR, 840 in India , 194 in Czechoslovakia )[source] | 24 built total[source] |
|---|
| Manufactured | 1959–1986[source] | 1987–1999[source] |
|---|
| Introduction date | 1959 (MiG-21F)[source] | 31 August 1998 (official)[source] |
|---|
| First flight | 14 February 1955 (Ye-2)[source] | 17 August 1987 ( 1987-08-17 )[source] |
|---|
| Variant | Chengdu J-7[source] | Shenyang J-15[source] |
|---|
| Guns | 1 × internal 23 mm Gryazev-Shipunov GSh-23 L autocannon with 200 rounds[source] | 1 × 30 mm Gryazev-Shipunov GSh-30-1 autocannon with 150 rounds[source] |
|---|
| 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:[source] | 12 × external hardpoints with a capacity of up to 6,500 kg (14,300 lb) of ordnance, with provisions to carry combinations of: Rockets: S-8 KOM/BM/OM S-13 T/OF S-25 OFM-PU Missiles: Air-to-air missiles : 8 × R-27 R/ER/T/ET 4 × R-73 E Anti-ship missiles : Kh-31 A Kh-41 Anti-radiation missiles : Kh-25 MP Kh-31 P Bombs: RBK-500 cluster bomb Up to 500 kg (1,100 lb) bombs[source] |
|---|
| Airfoil | root: TsAGI S-12 (4.2%); tip: TsAGI S-12 (5%)[source] | — |
|---|
| Landing speed | 250 km/h (160 mph; 130 kn)[source] | 240 km/h (150 mph; 130 kn)[source] |
|---|
| Time to altitude | 17,000 m (56,000 ft) in 8 minutes 30 seconds[source] | — |
|---|
| Thrust/weight | 0.76[source] | 0.83[source] |
|---|
| Take-off run | 830 m (2,720 ft)[source] | — |
|---|
| Landing run with SPS and brake parachute | 550 m (1,800 ft)[source] | — |
|---|
| Rockets | 4 × S-24 or 4× UB-16-57 rocket pods (4×16 57mm rockets)[source] | S-8 KOM/BM/OM S-13 T/OF S-25 OFM-PU[source] |
|---|
| Bombs | 2 × 500 kg (1,100 lb) and 2 × 250 kg bombs[source] | RBK-500 cluster bomb Up to 500 kg (1,100 lb) bombs[source] |
|---|
| Manufacturer | — | Sukhoi , Komsomolsk-on-Amur Aircraft Production Association[source] |
|---|
| Primary user | — | Russian Navy[source] |
|---|
| Developed from | — | Sukhoi Su-27[source] |
|---|
| Fuel capacity | — | 9,500 kg (20,900 lb) internal[source] |
|---|
| Stall speed | — | 240 km/h (150 mph, 130 kn)[source] |
|---|
| g limits | — | + 8[source] |
|---|
| Wing loading | — | 483 kg/m 2 (99 lb/sq ft)[source] |
|---|
| Missiles | — | Air-to-air missiles : 8 × R-27 R/ER/T/ET 4 × R-73 E Anti-ship missiles : Kh-31 A Kh-41 Anti-radiation missiles : Kh-25 MP Kh-31 P[source] |
|---|
| Reported operators |
| — |
|---|
Maximum take-off; Max takeoff weight
2 × Saturn AL-31F3 afterburning turbofan engines, 74.5 kN (16,700 lbf) thrust each dry, 125.5 kN (28,200 lbf) with afterburner[source]