Search filter

    • Year
      1906
      2018
    • Length
      11 m
      18 m
    • Height
      3 m
      5 m
    • Width
      1 m
      8 m
    • Diameter
      3 m
      9 m
    • Wing area
      18 m2
      28 m2
    • Wingspan (Beam)
      5 m
      9 m
    • Wing loading
      3 kg/m2
      829 kg/m2
    • Swept
      4 m
      10 m
    • Sweep
      25 deg
      68 deg
    • Aspect ratio
      1
      26
    • Disc area
      1 m2
      460 m2
    • Main rotor diameter
      1 m
      62 m
    • Rotor number
      1 qt
      8 qt
    • Blades per rotor
      4 qt
      5 qt
    • Disc loading
      17 kg/m2
      73 kg/m2
    • Tail rotor diameter
      0 m
      5 m
    • Empty weight
      4368 kg
      6552 kg
    • Max. takeoff weight (Gross weight)
      8080 kg
      12120 kg
    • Loaded weight
      7060 kg
      10590 kg
    • Crew
      1 per.
      2 per.
    • Useful load
      26 kg
      90700 kg
    • Payload
      23 kg
      122470 kg
    • Capacity passengers
      1 per.
      400 per.
    • Hardpoints
      1 qt
      2576 qt
    • Ground Speed
      1040 km/h
      1500 km/h
    • Max. Speed
      1740 km/h
      2610 km/h
    • Сruise Speed
      52 km/h
      3087 km/h
    • Stall Speed
      40 km/h
      258 km/h
    • Landing Speed
      68 km/h
      270 km/h
    • Minimum control speed
      24 km/h
      113 km/h
    • Never exceed speed
      107 km/h
      1050 km/h
    • Fuel Capacity
      3057 l
      4587 l
    • Fuel External
      142 l
      10025 l
    • Power/mass
      0 hp/kg
      23 hp/kg
    • Thrust/weight
      0 kN/kg
      3 kN/kg
    • Afterburning thrust
      55 kN/kg
      84 kN/kg
    • Total Power
      0 hp
      60000 hp
    • Thrust
      32 kN
      49 kN
    • Service ceiling
      14240 m
      21360 m
    • Static ceiling
      3 m
      5485 m
    • Range (Ferry range)
      968 km
      1452 km
    • Range PTB (Ferry range)
      720 km
      10000 km
    • Сombat radius
      277 km
      7210 km
    • Endurance
      0 h
      150 h
    • Takeoff roll
      20 m
      3200 m
    • Landing roll
      20 m
      2570 m
    • Maximum glide ratio
      7
      43
    • Load factor from
      6 G
      9 G
    • Rate of climb
      10800 m/min
      16200 m/min
    • Rate of sink
      36 m/min
      56 m/min
    • Time to altitude
      0 min
      105 min
    • Propellers
      1 qt
      8 qt
    • Prop diameter
      1 m
      6 m
    • Prop blade number
      1 qt
      8 qt
    • Guns
      2 qt
      4 qt
    • Bombs
      1 qt
      3 qt
    • Missiles
      1 qt
      24 qt
    • Rockets
      1 qt
      76 qt
    • Torpedoes
      1 qt
      4 qt
    • Bombs weight
      2 kg
      39000 kg
    • Rockets weight
      1 kg
      48 kg
    • Number built
      9196 qt
      13796 qt
    • Price
      41 USD
      750000000 USD

MiG MiG-21

TypeAircraft
Company

Russian Aircraft Corporation MiG

Scheme

Midwing

Monoplane

Geometry
Length (m)
1.9
 
14.5
88.7
Height (m)
0.6
 
4
50.1
Wings
Wing area (m2)
1.1
 
23
925
Wingspan (Beam) (m)
0.1
 
7.2
95
Weights
Empty weight (kg)
8
 
5,460
276,800
Max. takeoff weight (Gross weight) (kg)
154
 
10,100
575,000
Loaded weight (kg)
5
 
8,825
242,500
Capacity
Crew (per.)
1
 
1
112
Speeds
Ground Speed (km/h)
96.6
 
1,300
1,500
Max. Speed (km/h)
25
 
2,175
28,165
Fuel
Fuel Capacity (l)
23
 
3,822
320,000
Power
Afterburning thrust (kN/kg)
29.4
 
69.6
980
Thrust (kN)
1.5
 
40.2
1,914
Performance
Service ceiling (m)
0.6
 
17,800
161,544
Range (Ferry range) (km)
4
 
1,210
40,700
internal fuel
Dynamic Performance
Load factor from (G)
2
 
8.5
9
Rate of climb (m/min)
1.9
 
13,500
36,000
Combat
Guns (qt)
1
 
3
18
1x internal 23 mm GSh-23 cannon; 2x R-27R1 or R-27T or 4x Vympel R-77 or
Bombs (qt)
1
 
2
250
500 kg (1,102 lbs) bombs
Stat
Number built (qt)
0
 
11,496
43,000
Introduction 1971
First flight 14.02.1956

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