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    • Year
      1906
      2018
    • Length
      7 m
      12 m
    • Height
      2 m
      4 m
    • Width
      1 m
      8 m
    • Diameter
      3 m
      9 m
    • Wing area
      15 m2
      24 m2
    • Wingspan (Beam)
      8 m
      13 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
      2041 kg
      3062 kg
    • Max. takeoff weight (Gross weight)
      2781 kg
      4173 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
      456 km/h
      686 km/h
    • Сruise Speed
      374 km/h
      562 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
      2028 hp
      3043 hp
    • Thrust
      1 kN
      1914 kN
    • Service ceiling
      7200 m
      10800 m
    • Static ceiling
      3 m
      5485 m
    • Range (Ferry range)
      418 km
      628 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
      4 min
      6 min
    • Propellers
      1 qt
      8 qt
    • Prop diameter
      1 m
      6 m
    • Prop blade number
      1 qt
      8 qt
    • Guns
      8 qt
      12 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
      1 qt
      3 qt
    • Price
      41 USD
      750000000 USD

Curtiss XP-46

TypeAircraft
Company

Curtiss Aeroplane and Motor Company

Scheme

Low wing

Monoplane

Geometry
Length (m)
1.9
 
9.2
88.7
Height (m)
0.6
 
3.1
50.1
Wings
Wing area (m2)
1.1
 
19.3
925
Wingspan (Beam) (m)
0.1
 
10.5
95
Weights
Empty weight (kg)
8
 
2,551.5
276,800
Max. takeoff weight (Gross weight) (kg)
154
 
3,476.8
575,000
Capacity
Crew (per.)
1
 
1
112
Speeds
Max. Speed (km/h)
25
 
571
28,165
at 3720 m
Сruise Speed (km/h)
52
 
468
3,087
Power
Total Power (hp)
0.4
 
2,535.3
60,000
Performance
Service ceiling (m)
0.6
 
9,000
161,544
Range (Ferry range) (km)
4
 
523
40,700
Dynamic Performance
Time to altitude (min)
0.6
 
5
105
to 3750 m
Combat
Guns (qt)
1
 
10
18
.50 in (12.7 mm) synchronized machine guns in the forward fuselage; Provision for 8 × .30 in (7.62 mm) wing-mounted guns
Stat
Number built (qt)
0
 
2
43,000
Introduction 1941
First flight 15.02.1941

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