Search filter

    • Year
      1906
      2018
    • Length
      6 m
      11 m
    • Height
      2 m
      4 m
    • Width
      1 m
      8 m
    • Diameter
      3 m
      9 m
    • Wing area
      17 m2
      27 m2
    • Wingspan (Beam)
      0 m
      95 m
    • Wing loading
      69 kg/m2
      105 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
      845 kg
      1269 kg
    • Max. takeoff weight (Gross weight)
      1556 kg
      2336 kg
    • Loaded weight
      1632 kg
      2448 kg
    • Crew
      1 per.
      112 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
      213 km/h
      321 km/h
    • Max. Speed
      25 km/h
      28165 km/h
    • Сruise Speed
      188 km/h
      282 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
      386 km/h
      580 km/h
    • Fuel Capacity
      315 l
      473 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
      1 kN
      1914 kN
    • Service ceiling
      4280 m
      6420 m
    • Static ceiling
      3 m
      5485 m
    • Range (Ferry range)
      4 km
      40700 km
    • Range PTB (Ferry range)
      720 km
      10000 km
    • Сombat radius
      612 km
      918 km
    • Endurance
      2 h
      4 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
      273 m/min
      411 m/min
    • Rate of sink
      36 m/min
      56 m/min
    • Time to altitude
      9 min
      14 min
    • Propellers
      1 qt
      2 qt
    • Prop diameter
      2 m
      4 m
    • Prop blade number
      1 qt
      3 qt
    • Guns
      1 qt
      18 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
      184 qt
      276 qt
    • Price
      41 USD
      750000000 USD

North American Aviation NA-64 Yale

Company

North American Aviation

Scheme

Low wing

Monoplane

Geometry
Length (m)
1.9
 
8.6
88.7
Height (m)
0.6
 
2.7
50.1
Wings
Wing area (m2)
1.1
 
22.4
925
Wing loading (kg/m2)
3.1
 
86.7
829
3.1
 
86.7
829
Weights
Empty weight (kg)
8
 
1,057
276,800
Max. takeoff weight (Gross weight) (kg)
154
 
1,946
575,000
normal weight per NAA
Loaded weight (kg)
5
 
2,040
242,500
Speeds
Ground Speed (km/h)
96.6
 
267
1,500
Сruise Speed (km/h)
52
 
235
3,087
64% power
Never exceed speed (km/h)
108.0
 
483
1,050
Fuel
Fuel Capacity (l)
23
 
394
320,000
Performance
Service ceiling (m)
0.6
 
5,350
161,544
full load
Сombat radius (km)
277
 
765
7,210
Endurance (h)
0.0
 
2.8
150
at maximum speed
Dynamic Performance
Rate of climb (m/min)
1.9
 
342
36,000
Time to altitude (min)
0.6
 
11.4
105
to 3050 m
Propellers
Propellers (qt)
1
 
1
8
Prop diameter (m)
1.8
 
2.7
5.8
Prop blade number (qt)
1
 
2
8
Stat
Number built (qt)
0
 
230
43,000
First flight 12.02.1940
Stop production 01.10.1946

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