Search filter

    • Year
      1906
      2018
    • Length
      8 m
      13 m
    • Height
      2 m
      5 m
    • Width
      1 m
      8 m
    • Diameter
      3 m
      9 m
    • Wing area
      16 m2
      25 m2
    • Wingspan (Beam)
      8 m
      13 m
    • Wing loading
      192 kg/m2
      289 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
      2904 kg
      4356 kg
    • Max. takeoff weight (Gross weight)
      4884 kg
      7326 kg
    • Loaded weight
      4000 kg
      6000 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
      837 km/h
      1257 km/h
    • Max. Speed
      752 km/h
      1130 km/h
    • Сruise Speed
      680 km/h
      1020 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
      1136 l
      1704 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
      980 kN/kg
    • Total Power
      0 hp
      60000 hp
    • Thrust
      1 kN
      1914 kN
    • Service ceiling
      12400 m
      18600 m
    • Static ceiling
      3 m
      5485 m
    • Range (Ferry range)
      1068 km
      1602 km
    • Range PTB (Ferry range)
      720 km
      10000 km
    • Сombat radius
      277 km
      7210 km
    • Endurance
      0 h
      150 h
    • Takeoff roll
      484 m
      726 m
    • Landing roll
      604 m
      906 m
    • Maximum glide ratio
      7
      43
    • Load factor from
      2 G
      9 G
    • Rate of climb
      1344 m/min
      2016 m/min
    • Rate of sink
      36 m/min
      56 m/min
    • Time to altitude
      1 min
      3 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
      76 qt
    • Torpedoes
      1 qt
      4 qt
    • Bombs weight
      2 kg
      39000 kg
    • Rockets weight
      1 kg
      48 kg
    • Number built
      9600 qt
      14400 qt
    • Price
      41 USD
      750000000 USD

MiG MiG-15

TypeAircraft
Company

Russian Aircraft Corporation MiG

Scheme

Monoplane

Midwing

Geometry
Length (m)
1.9
 
10.1
88.7
Height (m)
0.6
 
3.7
50.1
Wings
Wing area (m2)
1.1
 
20.6
925
Wingspan (Beam) (m)
0.1
 
10.1
95
Wing loading (kg/m2)
3.1
 
240.8
829
Weights
Empty weight (kg)
8
 
3,630
276,800
Max. takeoff weight (Gross weight) (kg)
154
 
6,105
575,000
Loaded weight (kg)
5
 
5,000
242,500
Capacity
Crew (per.)
1
 
1
112
Speeds
Ground Speed (km/h)
96.6
 
1,047
1,500
Max. Speed (km/h)
25
 
1,021
28,165
at 5000 m
25
 
941
28,165
at 10000 m
Сruise Speed (km/h)
52
 
850
3,087
Fuel
Fuel Capacity (l)
23
 
1,420
320,000
Power
Thrust/weight (kN/kg)
0.0
 
0.0
2.1
Performance
Service ceiling (m)
0.6
 
15,500
161,544
Range (Ferry range) (km)
4
 
1,335
40,700
Takeoff roll (m)
20
 
605
3,200
Landing roll (m)
20
 
755
2,570
Dynamic Performance
Rate of climb (m/min)
1.9
 
966
36,000
at 10000 m
1.9
 
2,460
36,000
at sea level
1.9
 
1,680
36,000
at 5000 m
Time to altitude (min)
0.6
 
6.8
105
to 10000 m
0.6
 
2.4
105
to 5000 m
Combat
Guns (qt)
1
 
3
18
2x NR-23 23 mm (0.906 in) cannon in the lower left fuselage; 1x Nudelman N-37 37 mm (1.457 in) cannon in the lower right fuselage
Bombs (qt)
1
 
2
250
100 kg (220 lb) bombs, drop tanks, or unguided rockets
Stat
Number built (qt)
0
 
12,000
43,000
Introduction 1947
First flight 30.12.1947

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