Flat Wing Area
91.3237 m²
Flat Wing Aspect Ratio
10.46
Maximum Take-Off Weight
26.4512 t (paragliders: kg)
Pictures
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Aircraft Weight Variants
| Aircraft |
Maximum Take-Off Weight (t (paragliders: kg)) |
|
Hughes XF-11 |
26.4512 |
Similar airplanes
All data (20 fields)
- Name
- Hughes XF-11
- Manufacturer
- Hughes Aircraft
- Description
- The Hughes XF-11 (redesignated XR-11 in 1948) was a prototype military reconnaissance aircraft designed and flown by Howard Hughes and built by Hughes Aircraft Company for the United States Army Air Forces (USAAF).
- First Flight
- 1946-07-07
- Designer
- Stanley Bell
- Length (m)
- 19.9
- Cockpit Crew
- 2
- Max Speed (km/h)
- 724.2048
- Max Ceiling (m)
- 12801.6
- Rate of Climb (m/s)
- 5.08
- National Origin
- Canada
- Number Built
- 2
- Powerplant Description
- 2 × Pratt & Whitney R-4360-31 Wasp Major 28-cyl. air-cooled radial piston engines, 2237 kW (3000 hp) each
- Primary Users
- United States Army Air Forces
- Status
- Canceled
- Wikipedia Article (URL)
- en.wikipedia.org/wiki/Hughes_XF-11
- Flat Wing Span (m)
- 30.9
- Flat Wing Area (m²)
- 91.3237
- Flat Wing Aspect Ratio
- 10.46
- Number of Engines
- 2