Length
18.5928 m
Flat Wing Span
24.9936 m
Height
5.7912 m
Flat Wing Area
55.9276 m²
Max Speed
688.7992 km/h
Max Ceiling
12192 m
Number of Engines
2
Number Built
0
Maximum Take-Off Weight
21.2962 t (paragliders: kg)
Maximum Range
4828.032 km

Pictures

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Aircraft Weight Variants

Aircraft Maximum Take-Off Weight (t (paragliders: kg)) Maximum Range (km)
Curtiss XP-71 21.2962 4828.032

Similar airplanes

Name Aircraft Engine Length (m) Flat Wing Span (m) Max Seating
Sud-Ouest Bretagne 18.95 26.9 43 Compare
Mitsubishi Q2M Tai'yō 18.75 25 Compare
Fiat G.18 Fiat A.80 18.81 25 18 Compare
Bréguet 670T 18.74 24.86 18 Compare
Xi'an KJ-600 17.9832 24.9936 Compare
Douglas DC-2 18.5928 25.908 14 Compare
All data (19 fields)
Name
Curtiss XP-71
Manufacturer
Military designations USAAS/USAAF/USAF
Description
The Curtiss XP-71 was a 1941 American aircraft proposal by the Curtiss-Wright Corporation for an exceptionally large heavy fighter design.
Designer
Military designations USAAS/USAAF/USAF
Type
Heavy fighter; Escort fighter; Bomber-destroyer/interceptor
Length (m)
18.5928
Height (m)
5.7912
Cockpit Crew
2
Max Speed (km/h)
688.7992
Max Ceiling (m)
12192
Armament
; 1 × 75 mm (2.95 in) cannon 20rpg; 2 × 37 mm (1.46 in) cannon 60rpg
Number Built
0
Powerplant Description
2 × Pratt & Whitney R-4360-13 Wasp Major 28-cylinder air-cooled radial piston engines, 2573 kW (3450 hp) each
Primary Users
United States Army Air Forces
Status
Cancelled in 1943
Wikipedia Article (URL)
en.wikipedia.org/wiki/Curtiss_XP-71
Flat Wing Span (m)
24.9936
Flat Wing Area (m²)
55.9276
Number of Engines
2