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    • Year
      1906
      2018
    • Length
      6 m
      10 m
    • Height
      4 m
      8 m
    • Width
      1 m
      8 m
    • Diameter
      3 m
      9 m
    • Wing area
      16 m2
      26 m2
    • Wingspan (Beam)
      9 m
      14 m
    • Wing loading
      103 kg/m2
      155 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
      1690 kg
      2537 kg
    • Max. takeoff weight (Gross weight)
      2467 kg
      3702 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
      380 km/h
      570 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
      3 kN/kg
    • Afterburning thrust
      29 kN/kg
      980 kN/kg
    • Total Power
      760 hp
      1140 hp
    • Thrust
      1 kN
      1914 kN
    • Service ceiling
      6705 m
      10059 m
    • Static ceiling
      3 m
      5485 m
    • Range (Ferry range)
      1240 km
      1860 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
      1 qt
      76 qt
    • Torpedoes
      1 qt
      4 qt
    • Bombs weight
      144 kg
      216 kg
    • Rockets weight
      1 kg
      48 kg
    • Number built
      10 qt
      16 qt
    • Price
      41 USD
      750000000 USD

North American Aviation P-64

TypeAircraft
Company

North American Aviation

Scheme

Low wing

Monoplane

Geometry
Length (m)
1.9
 
8.2
88.7
Height (m)
0.6
 
6.0
50.1
Wings
Wing area (m2)
1.1
 
21.1
925
Wingspan (Beam) (m)
0.1
 
11.4
95
Wing loading (kg/m2)
3.1
 
129
829
Weights
Empty weight (kg)
8
 
2,113.7
276,800
Max. takeoff weight (Gross weight) (kg)
154
 
3,084.4
575,000
Capacity
Crew (per.)
1
 
1
112
Speeds
Max. Speed (km/h)
25
 
475
28,165
at 2650 m
Power
Total Power (hp)
0.4
 
950
60,000
1 powerplant
Performance
Service ceiling (m)
0.6
 
8,382
161,544
Range (Ferry range) (km)
4
 
1,550
40,700
Combat
Guns (qt)
1
 
6
18
4 × .30 in (7.62 mm) machine guns (2 synchronized in the nose, 1 in each wing); 2 × 20 mm cannons (Located in pods beneath each wing)
Bombs weight (kg)
2
 
180
39,000
Stat
Number built (qt)
0
 
13
43,000
Introduction 1939
First flight 01.05.1939
Stop production 1950

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