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    • Year
      1906
      2018
    • Length
      11 m
      18 m
    • Height
      3 m
      5 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
      4271 kg
      6407 kg
    • Max. takeoff weight (Gross weight)
      7680 kg
      11520 kg
    • Loaded weight
      7060 kg
      10590 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
      1040 km/h
      1500 km/h
    • Max. Speed
      1782 km/h
      2674 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
      3 kN/kg
    • Afterburning thrust
      111 kN/kg
      168 kN/kg
    • Total Power
      0 hp
      60000 hp
    • Thrust
      64 kN
      97 kN
    • Service ceiling
      14240 m
      21360 m
    • Static ceiling
      3 m
      5485 m
    • Range (Ferry range)
      968 km
      1452 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
      6 G
      9 G
    • Rate of climb
      10800 m/min
      16200 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
      2 qt
    • Bombs
      1 qt
      3 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
      0 qt
      43000 qt
    • Price
      41 USD
      750000000 USD

MiG A-144

TypeAircraft
Company

Russian Aircraft Corporation MiG

Scheme

Monoplane

Midwing

Geometry
Length (m)
1.9
 
14.5
88.7
Height (m)
0.6
 
4.1
50.1
Wings
Wing area (m2)
1.1
 
23
925
Wingspan (Beam) (m)
0.1
 
7.2
95
Weights
Empty weight (kg)
8
 
5,339
276,800
Max. takeoff weight (Gross weight) (kg)
154
 
9,600
575,000
Loaded weight (kg)
5
 
8,825
242,500
Capacity
Crew (per.)
1
 
1
112
Speeds
Ground Speed (km/h)
96.6
 
1,300
1,500
Max. Speed (km/h)
25
 
2,228
28,165
Power
Afterburning thrust (kN/kg)
29.4
 
139.2
980
2 powerplants 69,62 kN each
Thrust (kN)
1.5
 
80.4
1,914
2 powerplants 40,21 kN each
Performance
Service ceiling (m)
0.6
 
17,800
161,544
Range (Ferry range) (km)
4
 
1,210
40,700
internal fuel
Dynamic Performance
Load factor from (G)
2
 
8.5
9
Rate of climb (m/min)
1.9
 
13,500
36,000
Combat
Guns (qt)
1
 
1
18
internal 23 mm GSh-23 cannon
Bombs (qt)
1
 
2
250
500 kg (1,102 lbs) bombs
Stat
Introduction 1994

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