Search filter

    • Year
      1906
      2018
    • Length
      7 m
      12 m
    • Height
      3 m
      5 m
    • Width
      1 m
      8 m
    • Diameter
      3 m
      9 m
    • Wing area
      17 m2
      27 m2
    • Wingspan (Beam)
      9 m
      14 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
      2202 kg
      3304 kg
    • Max. takeoff weight (Gross weight)
      3196 kg
      4796 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
      464 km/h
      696 km/h
    • Сruise Speed
      344 km/h
      518 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
      920 hp
      1380 hp
    • Thrust
      1 kN
      1914 kN
    • Service ceiling
      7071 m
      10608 m
    • Static ceiling
      3 m
      5485 m
    • Range (Ferry range)
      880 km
      1320 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
      512 m/min
      769 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
      725 kg
      1089 kg
    • Rockets weight
      1 kg
      48 kg
    • Number built
      10990 qt
      16486 qt
    • Price
      35913 USD
      53871 USD

Curtiss P-40 Warhawk

TypeAircraft
Company

Curtiss Aeroplane and Motor Company

Scheme

Low wing

Monoplane

Geometry
Length (m)
1.9
 
9.7
88.7
Height (m)
0.6
 
3.8
50.1
Wings
Wing area (m2)
1.1
 
21.9
925
Wingspan (Beam) (m)
0.1
 
11.4
95
Weights
Empty weight (kg)
8
 
2,753.3
276,800
Max. takeoff weight (Gross weight) (kg)
154
 
3,996.2
575,000
Capacity
Crew (per.)
1
 
1
112
Speeds
Max. Speed (km/h)
25
 
580
28,165
Сruise Speed (km/h)
52
 
431
3,087
Power
Total Power (hp)
0.4
 
1,150
60,000
1 powerplant
Performance
Service ceiling (m)
0.6
 
8,839.2
161,544
Range (Ferry range) (km)
4
 
1,100
40,700
Dynamic Performance
Rate of climb (m/min)
1.9
 
640.1
36,000
Combat
Guns (qt)
1
 
6
18
.50 in (12.7 mm) M2 Browning machine guns with 235 rounds per gun in the wings
Bombs weight (kg)
2
 
907
39,000
Stat
Number built (qt)
0
 
13,738
43,000
Price (USD)
41.5
 
44,892
750.0 million
Introduction 1941
First flight 14.10.1938
Stop production 1958

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