Search filter

    • Year
      1906
      2018
    • Length
      10 m
      16 m
    • Height
      3 m
      6 m
    • Width
      1 m
      8 m
    • Diameter
      3 m
      9 m
    • Wing area
      30 m2
      46 m2
    • Wingspan (Beam)
      12 m
      19 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
      5816 kg
      8726 kg
    • Max. takeoff weight (Gross weight)
      9305 kg
      13959 kg
    • Loaded weight
      5 kg
      242500 kg
    • Crew
      1 per.
      3 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
      592 km/h
      888 km/h
    • Сruise Speed
      360 km/h
      542 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
      3 kN/kg
    • Afterburning thrust
      29 kN/kg
      980 kN/kg
    • Total Power
      2208 hp
      3312 hp
    • Thrust
      1 kN
      1914 kN
    • Service ceiling
      9485 m
      14229 m
    • Static ceiling
      3 m
      5485 m
    • Range (Ferry range)
      2884 km
      4326 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
      2 G
      9 G
    • Rate of climb
      1 m/min
      36000 m/min
    • Rate of sink
      36 m/min
      56 m/min
    • Time to altitude
      0 min
      105 min
    • Propellers
      1 qt
      8 qt
    • Prop diameter
      1 m
      6 m
    • Prop blade number
      1 qt
      8 qt
    • Guns
      4 qt
      8 qt
    • Bombs
      1 qt
      250 qt
    • Missiles
      1 qt
      24 qt
    • Rockets
      20 qt
      30 qt
    • Torpedoes
      1 qt
      4 qt
    • Bombs weight
      1440 kg
      2160 kg
    • Rockets weight
      1 kg
      48 kg
    • Number built
      217 qt
      327 qt
    • Price
      172123 USD
      258185 USD

North American Aviation F-82 Twin Mustang

TypeAircraft
Company

North American Aviation

Scheme

Low wing

Monoplane

Geometry
Length (m)
1.9
 
12.9
88.7
Height (m)
0.6
 
4.2
50.1
Wings
Wing area (m2)
1.1
 
37.9
925
Wingspan (Beam) (m)
0.1
 
15.6
95
Weights
Empty weight (kg)
8
 
7,271
276,800
Max. takeoff weight (Gross weight) (kg)
154
 
11,632
575,000
Capacity
Crew (per.)
1
 
2
112
Speeds
Max. Speed (km/h)
25
 
740
28,165
at 6400 m
Сruise Speed (km/h)
52
 
451
3,087
Power
Total Power (hp)
0.4
 
2,760
60,000
2 powerplants 1380 hp each
Performance
Service ceiling (m)
0.6
 
11,856.7
161,544
Range (Ferry range) (km)
4
 
3,605
40,700
Combat
Guns (qt)
1
 
6
18
.50 in (12.7 mm) Browning M3 machine guns
Rockets (qt)
1
 
25
76
5 in (127 mm) rockets
Bombs weight (kg)
2
 
1,800
39,000
Stat
Number built (qt)
0
 
272
43,000
Price (USD)
41.5
 
215,154
750.0 million
Introduction 1946
First flight 15.06.1945
Stop production 1953

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