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    • Year
      1906
      2018
    • Length
      15 m
      24 m
    • Height
      4 m
      8 m
    • Width
      1 m
      8 m
    • Diameter
      3 m
      9 m
    • Wing area
      49 m2
      75 m2
    • Wingspan (Beam)
      11 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
      16000 kg
      24000 kg
    • Max. takeoff weight (Gross weight)
      32960 kg
      49440 kg
    • Loaded weight
      5 kg
      242500 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
      96 km/h
      1500 km/h
    • Max. Speed
      960 km/h
      1440 km/h
    • Сruise Speed
      1876 km/h
      2814 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
      13264 l
      19896 l
    • Fuel External
      142 l
      10025 l
    • Power/mass
      0 hp/kg
      23 hp/kg
    • Thrust/weight
      0 kN/kg
      1 kN/kg
    • Afterburning thrust
      160 kN/kg
      241 kN/kg
    • Total Power
      0 hp
      60000 hp
    • Thrust
      117 kN
      177 kN
    • Service ceiling
      16560 m
      24840 m
    • Static ceiling
      3 m
      5485 m
    • Range (Ferry range)
      1384 km
      2076 km
    • Range PTB (Ferry range)
      720 km
      10000 km
    • Сombat radius
      277 km
      7210 km
    • Endurance
      0 h
      150 h
    • Takeoff roll
      960 m
      1440 m
    • Landing roll
      640 m
      960 m
    • Maximum glide ratio
      7
      43
    • Load factor from
      3 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
      3 qt
      5 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
      948 qt
      1424 qt
    • Price
      41 USD
      750000000 USD

MiG MiG-25

TypeAircraft
Company

Russian Aircraft Corporation MiG

Scheme

Monoplane

High wing

Geometry
Length (m)
1.9
 
19.8
88.7
Height (m)
0.6
 
6.1
50.1
Wings
Wing area (m2)
1.1
 
62.4
925
Wingspan (Beam) (m)
0.1
 
14.0
95
Weights
Empty weight (kg)
8
 
20,000
276,800
Max. takeoff weight (Gross weight) (kg)
154
 
41,200
575,000
Capacity
Crew (per.)
1
 
1
112
Speeds
Max. Speed (km/h)
25
 
3,470
28,165
continuous engine limit at high altitude
25
 
1,200
28,165
at altitude
Сruise Speed (km/h)
52
 
2,345
3,087
Fuel
Fuel Capacity (l)
23
 
16,580
320,000
Power
Thrust/weight (kN/kg)
0.0
 
0.7
2.1
Afterburning thrust (kN/kg)
29.4
 
200.2
980
2 powerplants 100,1 kN each
Thrust (kN)
1.5
 
147
1,914
2 powerplants 73,5 kN each
Performance
Service ceiling (m)
0.6
 
20,700
161,544
with four missiles
Range (Ferry range) (km)
4
 
1,730
40,700
with internal fuel
Takeoff roll (m)
20
 
1,200
3,200
Landing roll (m)
20
 
800
2,570
Dynamic Performance
Load factor from (G)
2
 
4.5
9
Rate of climb (m/min)
1.9
 
12,480
36,000
Combat
Guns (qt)
1
 
4
18
2x radar-guided R-40R (AA-6 "Acrid") air-to-air missiles; 2x infrared-guided R-40T missiles
Stat
Number built (qt)
0
 
1,186
43,000
Introduction 1977
First flight 06.03.1964

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