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    • Year
      1906
      2018
    • Length
      18 m
      28 m
    • Height
      4 m
      8 m
    • Width
      1 m
      8 m
    • Diameter
      3 m
      9 m
    • Wing area
      49 m2
      74 m2
    • Wingspan (Beam)
      10 m
      17 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
      17456 kg
      26184 kg
    • Max. takeoff weight (Gross weight)
      36960 kg
      55440 kg
    • Loaded weight
      5 kg
      242500 kg
    • Crew
      1 per.
      3 per.
    • Useful load
      26 kg
      90700 kg
    • Payload
      23 kg
      122470 kg
    • Capacity passengers
      1 per.
      400 per.
    • Hardpoints
      6 qt
      10 qt
    • Ground Speed
      96 km/h
      1500 km/h
    • Max. Speed
      2400 km/h
      3600 km/h
    • Сruise Speed
      2000 km/h
      3000 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
      23 l
      320000 l
    • Fuel External
      142 l
      10025 l
    • Power/mass
      0 hp/kg
      23 hp/kg
    • Thrust/weight
      0 kN/kg
      2 kN/kg
    • Afterburning thrust
      243 kN/kg
      365 kN/kg
    • Total Power
      0 hp
      60000 hp
    • Thrust
      148 kN
      224 kN
    • Service ceiling
      16480 m
      24720 m
    • Static ceiling
      3 m
      5485 m
    • Range (Ferry range)
      2400 km
      3600 km
    • Range PTB (Ferry range)
      720 km
      10000 km
    • Сombat radius
      1160 km
      1740 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
      4 G
      6 G
    • Rate of climb
      9984 m/min
      14976 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
      1 qt
      2 qt
    • Bombs
      1 qt
      250 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
      415 qt
      623 qt
    • Price
      41 USD
      750000000 USD

MiG MiG-31

TypeAircraft
Company

Russian Aircraft Corporation MiG

Scheme

Monoplane

High wing

Geometry
Length (m)
1.9
 
22.7
88.7
Height (m)
0.6
 
6.2
50.1
Wings
Wing area (m2)
1.1
 
61.6
925
Wingspan (Beam) (m)
0.1
 
13.5
95
Weights
Empty weight (kg)
8
 
21,820
276,800
Max. takeoff weight (Gross weight) (kg)
154
 
46,200
575,000
Capacity
Crew (per.)
1
 
2
112
pilot and weapons system officer
Hardpoints (qt)
1
 
8
2,576
6 for rockets and 2 for external fuel tanks
Speeds
Max. Speed (km/h)
25
 
3,000
28,165
High altitude
Сruise Speed (km/h)
52
 
2,500
3,087
Power
Thrust/weight (kN/kg)
0.0
 
0.9
2.1
Afterburning thrust (kN/kg)
29.4
 
304
980
2 powerplants 152 kN each
Thrust (kN)
1.5
 
186
1,914
2 powerplants 93 kN each
Performance
Service ceiling (m)
0.6
 
20,600
161,544
Range (Ferry range) (km)
4
 
3,000
40,700
Сombat radius (km)
277
 
1,450
7,210
Dynamic Performance
Load factor from (G)
2
 
5
9
Rate of climb (m/min)
1.9
 
12,480
36,000
Combat
Guns (qt)
1
 
1
18
GSh-6-23 23 mm cannon with 260 rounds.
Stat
Number built (qt)
0
 
519
43,000
Introduction 1985
First flight 16.09.1975

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