Search filter

    • Year
      1906
      2018
    • Length
      9 m
      14 m
    • Height
      3 m
      5 m
    • Width
      1 m
      8 m
    • Diameter
      3 m
      9 m
    • Wing area
      18 m2
      28 m2
    • Wingspan (Beam)
      7 m
      12 m
    • Wing loading
      189 kg/m2
      285 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
      3135 kg
      4703 kg
    • Max. takeoff weight (Gross weight)
      4855 kg
      7283 kg
    • Loaded weight
      5 kg
      242500 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
      916 km/h
      1374 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
      1 kN/kg
    • Afterburning thrust
      29 kN/kg
      41 kN/kg
    • Total Power
      0 hp
      60000 hp
    • Thrust
      21 kN
      32 kN
    • Service ceiling
      13280 m
      19920 m
    • Static ceiling
      3 m
      5485 m
    • Range (Ferry range)
      1648 km
      2472 km
    • Range PTB (Ferry range)
      720 km
      10000 km
    • Сombat radius
      277 km
      7210 km
    • Endurance
      0 h
      150 h
    • Takeoff roll
      440 m
      660 m
    • Landing roll
      680 m
      1020 m
    • Maximum glide ratio
      7
      43
    • Load factor from
      6 G
      9 G
    • Rate of climb
      3120 m/min
      4680 m/min
    • Rate of sink
      36 m/min
      56 m/min
    • Time to altitude
      11 min
      18 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
      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
      8848 qt
      13272 qt
    • Price
      41 USD
      750000000 USD

MiG MiG-17

TypeAircraft
Company

Russian Aircraft Corporation MiG

Scheme

Midwing

Monoplane

Geometry
Length (m)
1.9
 
11.3
88.7
Height (m)
0.6
 
3.8
50.1
Wings
Wing area (m2)
1.1
 
22.6
925
Wingspan (Beam) (m)
0.1
 
9.6
95
Wing loading (kg/m2)
3.1
 
237
829
Weights
Empty weight (kg)
8
 
3,919
276,800
Max. takeoff weight (Gross weight) (kg)
154
 
6,069
575,000
Capacity
Crew (per.)
1
 
1
112
Speeds
Max. Speed (km/h)
25
 
1,070
28,165
at 5000 m
25
 
1,145
28,165
at 3000 m
Power
Thrust/weight (kN/kg)
0.0
 
0.5
2.1
Afterburning thrust (kN/kg)
29.4
 
33.8
980
1 powerplant
Thrust (kN)
1.5
 
26.5
1,914
1 powerplant
Performance
Service ceiling (m)
0.6
 
16,600
161,544
Range (Ferry range) (km)
4
 
2,060
40,700
with drop tanks
Takeoff roll (m)
20
 
550
3,200
Landing roll (m)
20
 
850
2,570
Dynamic Performance
Load factor from (G)
2
 
8
9
Rate of climb (m/min)
1.9
 
3,900
36,000
Time to altitude (min)
0.6
 
3
105
to 5000 m
0.6
 
6.7
105
to 10000 m
0.6
 
14.3
105
to 15000 m
Combat
Guns (qt)
1
 
3
18
1x 37 mm Nudelman N-37 cannon; 2x 23 mm Nudelman-Rikhter NR-23 cannons
Stat
Number built (qt)
0
 
11,060
43,000
Introduction 1953
First flight 14.01.1950

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