Search filter

    • Year
      1906
      2018
    • Length
      7 m
      12 m
    • Height
      2 m
      4 m
    • Width
      1 m
      8 m
    • Diameter
      3 m
      9 m
    • Wing area
      14 m2
      22 m2
    • Wingspan (Beam)
      8 m
      12 m
    • Wing loading
      222 kg/m2
      334 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
      2680 kg
      4020 kg
    • Max. takeoff weight (Gross weight)
      154 kg
      575000 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
      691 km/h
      1037 km/h
    • Max. Speed
      732 km/h
      1098 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
      840 km/h
      1050 km/h
    • Fuel Capacity
      1300 l
      1950 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
      12 kN
      19 kN
    • Service ceiling
      10800 m
      16200 m
    • Static ceiling
      3 m
      5485 m
    • Range (Ferry range)
      640 km
      960 km
    • Range PTB (Ferry range)
      720 km
      10000 km
    • Сombat radius
      277 km
      7210 km
    • Endurance
      0 h
      150 h
    • Takeoff roll
      760 m
      1140 m
    • Landing roll
      848 m
      1272 m
    • Maximum glide ratio
      7
      43
    • Load factor from
      2 G
      9 G
    • Rate of climb
      1056 m/min
      1584 m/min
    • Rate of sink
      36 m/min
      56 m/min
    • Time to altitude
      8 min
      13 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
      488 qt
      732 qt
    • Price
      41 USD
      750000000 USD

MiG MiG-9

TypeAircraft
Company

Russian Aircraft Corporation MiG

Scheme

Monoplane

Midwing

Geometry
Length (m)
1.9
 
9.8
88.7
Height (m)
0.6
 
3.2
50.1
Wings
Wing area (m2)
1.1
 
18.2
925
Wingspan (Beam) (m)
0.1
 
10
95
Wing loading (kg/m2)
3.1
 
278
829
Weights
Empty weight (kg)
8
 
3,350
276,800
Loaded weight (kg)
5
 
5,000
242,500
Capacity
Crew (per.)
1
 
1
112
Speeds
Ground Speed (km/h)
96.6
 
864
1,500
Max. Speed (km/h)
25
 
915
28,165
Never exceed speed (km/h)
108.0
 
1,050
1,050
Fuel
Fuel Capacity (l)
23
 
1,625
320,000
Power
Thrust (kN)
1.5
 
15.6
1,914
2 powerplants 7,8 kN each
Performance
Service ceiling (m)
0.6
 
13,500
161,544
Range (Ferry range) (km)
4
 
800
40,700
at 10000 m
Takeoff roll (m)
20
 
950
3,200
with total weight of 4950 kg
Landing roll (m)
20
 
1,060
2,570
with total weight of 3760 kg
Dynamic Performance
Rate of climb (m/min)
1.9
 
1,320
36,000
Time to altitude (min)
0.6
 
4.3
105
to 5000 m
0.6
 
10.8
105
to 10000 m
Combat
Guns (qt)
1
 
3
18
1 × 37 mm Nudelman N-37 cannon; 2 × 23 mm Nudelman-Suranov NS-23 cannon
Stat
Number built (qt)
0
 
610
43,000
Introduction 1949
First flight 24.04.1946

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