Search filter

    • Year
      1906
      2018
    • Length
      14 m
      22 m
    • Height
      0 m
      51 m
    • Width
      1 m
      8 m
    • Diameter
      3 m
      9 m
    • Wing area
      25 m2
      39 m2
    • Wingspan (Beam)
      7 m
      12 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
      6619 kg
      9929 kg
    • Max. takeoff weight (Gross weight)
      9176 kg
      13764 kg
    • Loaded weight
      8760 kg
      13140 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
      1640 km/h
      2460 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
      1600 l
      2400 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
      29 kN/kg
      980 kN/kg
    • Total Power
      0 hp
      60000 hp
    • Thrust
      49 kN
      74 kN
    • Service ceiling
      16800 m
      25200 m
    • Static ceiling
      3 m
      5485 m
    • Range (Ferry range)
      1176 km
      1764 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
      7 G
      9 G
    • Rate of climb
      1 m/min
      36000 m/min
    • Rate of sink
      36 m/min
      56 m/min
    • Time to altitude
      2 min
      4 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
      0 qt
      43000 qt
    • Price
      41 USD
      750000000 USD

MiG I-75

TypeAircraft
Company

Russian Aircraft Corporation MiG

Scheme

Monoplane

Midwing

Geometry
Length (m)
1.9
 
18.3
88.7
Wings
Wing area (m2)
1.1
 
31.9
925
Wingspan (Beam) (m)
0.1
 
10.0
95
Weights
Empty weight (kg)
8
 
8,274
276,800
Max. takeoff weight (Gross weight) (kg)
154
 
11,470
575,000
Loaded weight (kg)
5
 
10,950
242,500
Capacity
Crew (per.)
1
 
1
112
Speeds
Max. Speed (km/h)
25
 
2,050
28,165
at 11400 m
Fuel
Fuel Capacity (l)
23
 
2,000
320,000
Power
Thrust (kN)
1.5
 
61.6
1,914
1 powerplant
Performance
Service ceiling (m)
0.6
 
21,000
161,544
Range (Ferry range) (km)
4
 
1,470
40,700
at 12000 m
Dynamic Performance
Load factor from (G)
2
 
9
9
Time to altitude (min)
0.6
 
0.9
105
to 6000 m
0.6
 
3.1
105
to 11000 m
Combat
Missiles (qt)
1
 
2
24
Kaliningrad K-8
Stat
Introduction 1958
First flight 1958

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