Search filter

    • Year
      1906
      2018
    • Length
      10 m
      16 m
    • Height
      3 m
      5 m
    • Width
      1 m
      8 m
    • Diameter
      3 m
      9 m
    • Wing area
      20 m2
      31 m2
    • Wingspan (Beam)
      7 m
      11 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
      4357 kg
      6537 kg
    • Max. takeoff weight (Gross weight)
      154 kg
      575000 kg
    • Loaded weight
      6048 kg
      9072 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
      1164 km/h
      1746 km/h
    • Сruise Speed
      52 km/h
      3087 km/h
    • Stall Speed
      40 km/h
      258 km/h
    • Landing Speed
      188 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
      2952 l
      4428 l
    • Fuel External
      142 l
      10025 l
    • Power/mass
      0 hp/kg
      23 hp/kg
    • Thrust/weight
      0 kN/kg
      2 kN/kg
    • Afterburning thrust
      50 kN/kg
      77 kN/kg
    • Total Power
      0 hp
      60000 hp
    • Thrust
      40 kN
      62 kN
    • Service ceiling
      14000 m
      21000 m
    • Static ceiling
      3 m
      5485 m
    • Range (Ferry range)
      1112 km
      1668 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
      8640 m/min
      12960 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
      2 qt
      4 qt
    • Bombs
      1 qt
      3 qt
    • Missiles
      1 qt
      24 qt
    • Rockets
      1 qt
      3 qt
    • Torpedoes
      1 qt
      4 qt
    • Bombs weight
      2 kg
      39000 kg
    • Rockets weight
      1 kg
      48 kg
    • Number built
      1737 qt
      2607 qt
    • Price
      41 USD
      750000000 USD

MiG MiG-19

TypeAircraft
Company

Russian Aircraft Corporation MiG

Scheme

Monoplane

Midwing

Geometry
Length (m)
1.9
 
12.5
88.7
less pitot boom
Height (m)
0.6
 
3.9
50.1
Wings
Wing area (m2)
1.1
 
25.2
925
Wingspan (Beam) (m)
0.1
 
9
95
Weights
Empty weight (kg)
8
 
5,447
276,800
Loaded weight (kg)
5
 
7,560
242,500
Capacity
Crew (per.)
1
 
1
112
Speeds
Max. Speed (km/h)
25
 
1,455
28,165
at 10000 m
Landing Speed (km/h)
68
 
235
270
Fuel
Fuel Capacity (l)
23
 
3,690
320,000
internal:2,170 l; drop tanks 2x 760 l
Power
Thrust/weight (kN/kg)
0.0
 
0.9
2.1
Afterburning thrust (kN/kg)
29.4
 
63.6
980
2 powerplants 31,8 kN each
Thrust (kN)
1.5
 
51
1,914
2 powerplants 25,5 kN each dry
Performance
Service ceiling (m)
0.6
 
17,500
161,544
wet
Range (Ferry range) (km)
4
 
1,390
40,700
Dynamic Performance
Load factor from (G)
2
 
8
9
Rate of climb (m/min)
1.9
 
10,800
36,000
Time to altitude (min)
0.6
 
1.1
105
to 10000 m
0.6
 
2.6
105
to 15000 m
Combat
Guns (qt)
1
 
3
18
30 millimetres (1.181 in) Nudelman-Rikhter NR-30 cannon
Bombs (qt)
1
 
2
250
50–250 kg
Rockets (qt)
1
 
2
76
FFAR rocket pods or
Stat
Number built (qt)
0
 
2,172
43,000
Introduction 1957
First flight 18.09.1953

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