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    • Year
      1906
      2018
    • Length
      13 m
      21 m
    • Height
      4 m
      6 m
    • Width
      1 m
      8 m
    • Diameter
      3 m
      9 m
    • Wing area
      1 m2
      925 m2
    • Wingspan (Beam)
      0 m
      95 m
    • Wing loading
      484 kg/m2
      726 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
      9526 kg
      14290 kg
    • Max. takeoff weight (Gross weight)
      16536 kg
      24804 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
      5 qt
      9 qt
    • Ground Speed
      1080 km/h
      1500 km/h
    • Max. Speed
      1508 km/h
      2262 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
      23 l
      320000 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
      90 kN/kg
      136 kN/kg
    • Total Power
      0 hp
      60000 hp
    • Thrust
      1 kN
      1914 kN
    • Service ceiling
      11200 m
      16800 m
    • Static ceiling
      3 m
      5485 m
    • Range (Ferry range)
      2000 km
      3000 km
    • Range PTB (Ferry range)
      720 km
      10000 km
    • Сombat radius
      432 km
      648 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
      5 G
      9 G
    • Rate of climb
      9600 m/min
      14400 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
      18 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
      860 qt
      1290 qt
    • Price
      41 USD
      750000000 USD

MiG MiG-27

TypeAircraft
Company

Russian Aircraft Corporation MiG

Scheme

High wing

Monoplane

Geometry
Length (m)
1.9
 
17.1
88.7
Height (m)
0.6
 
5
50.1
Wings
Wing loading (kg/m2)
3.1
 
605
829
Weights
Empty weight (kg)
8
 
11,908
276,800
Max. takeoff weight (Gross weight) (kg)
154
 
20,670
575,000
Capacity
Crew (per.)
1
 
1
112
Hardpoints (qt)
1
 
1
2,576
1
 
7
2,576
Speeds
Ground Speed (km/h)
96.6
 
1,350
1,500
Max. Speed (km/h)
25
 
1,885
28,165
at 8000 m
Power
Thrust/weight (kN/kg)
0.0
 
0.6
2.1
Afterburning thrust (kN/kg)
29.4
 
112.8
980
1 powerplant
Performance
Service ceiling (m)
0.6
 
14,000
161,544
Range (Ferry range) (km)
4
 
2,500
40,700
Ferry range
Сombat radius (km)
277
 
780
7,210
with two Kh-29 ASMs and three drop tanks lo-lo-lo
277
 
540
7,210
with two Kh-29 ASMs and no external fuel lo-lo-lo
Dynamic Performance
Load factor from (G)
2
 
7
9
Rate of climb (m/min)
1.9
 
12,000
36,000
Stat
Number built (qt)
0
 
1,075
43,000
Introduction 1976
First flight 20.08.1970

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