Search filter

    • Year
      1906
      2018
    • Length
      11 m
      18 m
    • Height
      0 m
      51 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
      4536 kg
      6804 kg
    • Max. takeoff weight (Gross weight)
      6560 kg
      9840 kg
    • Loaded weight
      5440 kg
      8160 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
      1784 km/h
      2676 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
      2560 l
      3840 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
      56 kN/kg
      85 kN/kg
    • Total Power
      0 hp
      60000 hp
    • Thrust
      36 kN
      56 kN
    • Service ceiling
      16000 m
      24000 m
    • Static ceiling
      3 m
      5485 m
    • Range (Ferry range)
      4 km
      40700 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
      2 G
      9 G
    • Rate of climb
      1 m/min
      36000 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
      3 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
      1 qt
      3 qt
    • Price
      41 USD
      750000000 USD

MiG Ye-8

TypeAircraft
Company

Russian Aircraft Corporation MiG

Scheme

Monoplane

Midwing

Geometry
Length (m)
1.9
 
14.9
88.7
Wings
Wing area (m2)
1.1
 
23.1
925
Wingspan (Beam) (m)
0.1
 
7.2
95
Weights
Empty weight (kg)
8
 
5,670
276,800
Max. takeoff weight (Gross weight) (kg)
154
 
8,200
575,000
Loaded weight (kg)
5
 
6,800
242,500
Capacity
Crew (per.)
1
 
1
112
Speeds
Max. Speed (km/h)
25
 
2,230
28,165
at 12000 m
Fuel
Fuel Capacity (l)
23
 
3,200
320,000
Power
Afterburning thrust (kN/kg)
29.4
 
70.6
980
1 powerplant
Thrust (kN)
1.5
 
46.1
1,914
1 powerplant
Performance
Service ceiling (m)
0.6
 
20,000
161,544
Combat
Missiles (qt)
1
 
2
24
Vympel K-13 air-to-air missiles (planned)
Stat
Number built (qt)
0
 
2
43,000
Introduction 1962
First flight 1962

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