Search filter

    • Year
      1906
      2018
    • Length
      9 m
      15 m
    • Height
      3 m
      6 m
    • Width
      1 m
      8 m
    • Diameter
      3 m
      9 m
    • Wing area
      1 m2
      925 m2
    • Wingspan (Beam)
      13 m
      20 m
    • Wing loading
      136 kg/m2
      206 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
      4272 kg
      6409 kg
    • Max. takeoff weight (Gross weight)
      6042 kg
      9064 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
      576 km/h
      866 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
      1840 hp
      2760 hp
    • Thrust
      1 kN
      1914 kN
    • Service ceiling
      8705 m
      13058 m
    • Static ceiling
      3 m
      5485 m
    • Range (Ferry range)
      1920 km
      2880 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
      3 qt
      5 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
      0 qt
      2 qt
    • Price
      41 USD
      750000000 USD

Curtiss P-62

TypeAircraft
Company

Curtiss Aeroplane and Motor Company

Scheme

Monoplane

Low wing

Geometry
Length (m)
1.9
 
12.0
88.7
Height (m)
0.6
 
5.0
50.1
Wings
Wingspan (Beam) (m)
0.1
 
16.4
95
Wing loading (kg/m2)
3.1
 
171
829
Weights
Empty weight (kg)
8
 
5,340.1
276,800
Max. takeoff weight (Gross weight) (kg)
154
 
7,552.8
575,000
Capacity
Crew (per.)
1
 
1
112
Speeds
Max. Speed (km/h)
25
 
721
28,165
Power
Total Power (hp)
0.4
 
2,300
60,000
1 powerplant
Performance
Service ceiling (m)
0.6
 
10,881.4
161,544
Range (Ferry range) (km)
4
 
2,400
40,700
Combat
Guns (qt)
1
 
4
18
20 mm (0.79 in) cannon
Stat
Number built (qt)
0
 
1
43,000
First flight 21.07.1943

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