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    • Year
      1906
      2018
    • Length
      15 m
      23 m
    • Height
      4 m
      7 m
    • Width
      1 m
      8 m
    • Diameter
      3 m
      9 m
    • Wing area
      1 m2
      925 m2
    • Wingspan (Beam)
      20 m
      31 m
    • Wing loading
      201 kg/m2
      303 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
      11270 kg
      16907 kg
    • Max. takeoff weight (Gross weight)
      17036 kg
      25556 kg
    • Loaded weight
      5 kg
      242500 kg
    • Crew
      1 per.
      3 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
      552 km/h
      828 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
      5520 hp
      8280 hp
    • Thrust
      1 kN
      1914 kN
    • Service ceiling
      9753 m
      14631 m
    • Static ceiling
      3 m
      5485 m
    • Range (Ferry range)
      3840 km
      5760 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
      10 min
      15 min
    • Propellers
      1 qt
      8 qt
    • Prop diameter
      1 m
      6 m
    • Prop blade number
      1 qt
      8 qt
    • Guns
      2 qt
      4 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
      43000 qt
    • Price
      41 USD
      750000000 USD

Curtiss XP-71

TypeAircraft
Company

Curtiss Aeroplane and Motor Company

Scheme

Monoplane

High wing

Geometry
Length (m)
1.9
 
18.9
88.7
Height (m)
0.6
 
5.8
50.1
Wings
Wingspan (Beam) (m)
0.1
 
25.1
95
Wing loading (kg/m2)
3.1
 
252
829
Weights
Empty weight (kg)
8
 
14,088.6
276,800
Max. takeoff weight (Gross weight) (kg)
154
 
21,296.2
575,000
Capacity
Crew (per.)
1
 
2
112
Speeds
Max. Speed (km/h)
25
 
690
28,165
at 7620 m
Power
Total Power (hp)
0.4
 
6,900
60,000
2 powerplants 2450 hp each
Performance
Service ceiling (m)
0.6
 
12,192
161,544
Range (Ferry range) (km)
4
 
4,800
40,700
Dynamic Performance
Time to altitude (min)
0.6
 
12.5
105
to 7620
Combat
Guns (qt)
1
 
3
18
1× 75 mm (2.95 in) cannon; 2× 37 mm (1.46 in) cannon
Stat

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