Search filter

    • Year
      1906
      2018
    • Length
      9 m
      15 m
    • Height
      3 m
      6 m
    • Width
      1 m
      8 m
    • Diameter
      3 m
      9 m
    • Wing area
      14 m2
      22 m2
    • Wingspan (Beam)
      8 m
      13 m
    • Wing loading
      3 kg/m2
      829 kg/m2
    • Swept
      4 m
      10 m
    • Sweep
      25 deg
      68 deg
    • Aspect ratio
      4
      7
    • 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
      8 kg
      276800 kg
    • Max. takeoff weight (Gross weight)
      6240 kg
      9360 kg
    • Loaded weight
      3688 kg
      5532 kg
    • Crew
      1 per.
      3 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
      96 km/h
      1500 km/h
    • Max. Speed
      800 km/h
      1200 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
      1912 l
      2868 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
      27 kN
      42 kN
    • Service ceiling
      11200 m
      16800 m
    • Static ceiling
      3 m
      5485 m
    • Range (Ferry range)
      960 km
      1440 km
    • Range PTB (Ferry range)
      1600 km
      2400 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
      6 G
      9 G
    • Rate of climb
      3921 m/min
      5883 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
      1 qt
      3 qt
    • Price
      41 USD
      750000000 USD

MiG MiG-AT

TypeAircraft
Company

Russian Aircraft Corporation MiG

Scheme

Monoplane

Low wing

Geometry
Length (m)
1.9
 
12.0
88.7
Height (m)
0.6
 
4.4
50.1
Wings
Wing area (m2)
1.1
 
17.7
925
Wingspan (Beam) (m)
0.1
 
10.2
95
Aspect ratio
1.7
 
5.7
25.6
Weights
Max. takeoff weight (Gross weight) (kg)
154
 
7,800
575,000
combat
Loaded weight (kg)
5
 
4,610
242,500
training
Capacity
Crew (per.)
1
 
2
112
Hardpoints (qt)
1
 
7
2,576
with a capacity of 2,000 kg
Speeds
Max. Speed (km/h)
25
 
1,000
28,165
at 2500 m
Fuel
Fuel Capacity (l)
23
 
2,390
320,000
Power
Thrust (kN)
1.5
 
34.5
1,914
2 powerplants 17,27 kN each
Performance
Service ceiling (m)
0.6
 
14,000
161,544
Range (Ferry range) (km)
4
 
1,200
40,700
Range PTB (Ferry range) (km)
720
 
2,000
10,000
Dynamic Performance
Load factor from (G)
2
 
8
9
Rate of climb (m/min)
1.9
 
4,902
36,000
Stat
Number built (qt)
0
 
2
43,000
Introduction 1996
First flight 16.03.1996

Similar aircraft

Get more

Comments