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    • Year
      1906
      2018
    • Length
      6 m
      10 m
    • Height
      2 m
      4 m
    • Width
      1 m
      8 m
    • Diameter
      3 m
      9 m
    • Wing area
      13 m2
      21 m2
    • Wingspan (Beam)
      8 m
      13 m
    • Wing loading
      142 kg/m2
      214 kg/m2
    • Swept
      4 m
      10 m
    • Sweep
      25 deg
      68 deg
    • Aspect ratio
      4
      8
    • 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
      2081 kg
      3123 kg
    • Max. takeoff weight (Gross weight)
      154 kg
      575000 kg
    • Loaded weight
      2479 kg
      3719 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
      388 km/h
      584 km/h
    • Max. Speed
      525 km/h
      789 km/h
    • Сruise Speed
      372 km/h
      560 km/h
    • Stall Speed
      40 km/h
      258 km/h
    • Landing Speed
      112 km/h
      170 km/h
    • Minimum control speed
      24 km/h
      113 km/h
    • Never exceed speed
      107 km/h
      1050 km/h
    • Fuel Capacity
      323 l
      485 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
      1080 hp
      1620 hp
    • Thrust
      1 kN
      1914 kN
    • Service ceiling
      9600 m
      14400 m
    • Static ceiling
      3 m
      5485 m
    • Range (Ferry range)
      464 km
      696 km
    • Range PTB (Ferry range)
      720 km
      10000 km
    • Сombat radius
      277 km
      7210 km
    • Endurance
      0 h
      150 h
    • Takeoff roll
      190 m
      286 m
    • Landing roll
      320 m
      480 m
    • Maximum glide ratio
      7
      43
    • Load factor from
      2 G
      9 G
    • Rate of climb
      806 m/min
      1210 m/min
    • Rate of sink
      36 m/min
      56 m/min
    • Time to altitude
      4 min
      8 min
    • Propellers
      1 qt
      2 qt
    • Prop diameter
      2 m
      4 m
    • Prop blade number
      2 qt
      4 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
      160 kg
      240 kg
    • Rockets weight
      1 kg
      48 kg
    • Number built
      82 qt
      124 qt
    • Price
      41 USD
      750000000 USD

MiG MiG-1

TypeAircraft
Company

Russian Aircraft Corporation MiG

Scheme

Low wing

Monoplane

Geometry
Length (m)
1.9
 
8.2
88.7
Height (m)
0.6
 
3.3
50.1
Wings
Wing area (m2)
1.1
 
17.4
925
Wingspan (Beam) (m)
0.1
 
10.2
95
Wing loading (kg/m2)
3.1
 
177.7
829
Aspect ratio
1.7
 
6.0
25.6
Weights
Empty weight (kg)
8
 
2,602
276,800
Loaded weight (kg)
5
 
3,099
242,500
Capacity
Crew (per.)
1
 
1
112
Speeds
Ground Speed (km/h)
96.6
 
486
1,500
Max. Speed (km/h)
25
 
657
28,165
Сruise Speed (km/h)
52
 
466
3,087
Landing Speed (km/h)
68
 
141
270
Fuel
Fuel Capacity (l)
23
 
404
320,000
Power
Total Power (hp)
0.4
 
1,350
60,000
1 powerplant
Performance
Service ceiling (m)
0.6
 
12,000
161,544
Range (Ferry range) (km)
4
 
580
40,700
Takeoff roll (m)
20
 
238
3,200
Landing roll (m)
20
 
400
2,570
Dynamic Performance
Rate of climb (m/min)
1.9
 
1,008
36,000
Time to altitude (min)
0.6
 
5.9
105
to 5000 m
Propellers
Propellers (qt)
1
 
1
8
Prop diameter (m)
1.8
 
3
5.8
Prop blade number (qt)
1
 
3
8
Combat
Guns (qt)
1
 
3
18
1 × 12.7 mm BS machine gun; 2 × 7.62 mm ShKAS machine guns
Bombs weight (kg)
2
 
200
39,000
Stat
Number built (qt)
0
 
103
43,000
including 3 prototypes
Introduction 1940
First flight 05.04.1940
Stop production 1943

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