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    • Year
      1906
      2018
    • Length
      8 m
      14 m
    • Height
      4 m
      7 m
    • Width
      1 m
      8 m
    • Diameter
      3 m
      9 m
    • Wing area
      27 m2
      42 m2
    • Wingspan (Beam)
      11 m
      17 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
      3821 kg
      5733 kg
    • Max. takeoff weight (Gross weight)
      5424 kg
      8138 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
      509 km/h
      765 km/h
    • Сruise Speed
      221 km/h
      333 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
      9704 m
      14558 m
    • Static ceiling
      3 m
      5485 m
    • Range (Ferry range)
      1969 km
      2955 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
      658 m/min
      988 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-Wright XF14C

TypeAircraft
Company

Curtiss-Wright

Scheme

Low wing

Monoplane

Geometry
Length (m)
1.9
 
11.1
88.7
Height (m)
0.6
 
5.2
50.1
Wings
Wing area (m2)
1.1
 
34.8
925
Wingspan (Beam) (m)
0.1
 
14.0
95
Weights
Empty weight (kg)
8
 
4,776.8
276,800
Max. takeoff weight (Gross weight) (kg)
154
 
6,781.2
575,000
Capacity
Crew (per.)
1
 
1
112
Speeds
Max. Speed (km/h)
25
 
637
28,165
at 9800 m
Сruise Speed (km/h)
52
 
277
3,087
Power
Total Power (hp)
0.4
 
2,300
60,000
1 powerplant
Performance
Service ceiling (m)
0.6
 
12,131.0
161,544
Range (Ferry range) (km)
4
 
2,462
40,700
Dynamic Performance
Rate of climb (m/min)
1.9
 
823.0
36,000
Combat
Guns (qt)
1
 
4
18
wing mounted 20 mm cannon (planned)
Stat
Number built (qt)
0
 
1
43,000
Introduction 1943
First flight 01.07.1944

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