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Aviation / Aerospace

Hughes XR-11 / XF-11


Long-Range Photographic Reconnaissance Aircraft Prototype [ 1946 ]



The Hughes XF-11 reconnaissance-minded platform only saw two prototypes completed - the first crashing into the suburb of Beverly Hills with Howard Hughes at the controls.



Authored By: Staff Writer | Last Edited: 06/28/2018 | Content ©www.MilitaryFactory.com | The following text is exclusive to this site.

VIEW SPECIFICATIONS [+]
Though only achieving prototype form, the XF-11 was one of the darling designs of famed American aviator Howard Hughes. Looking very much like an oversized Lockheed P-38, the twin-boom XF-11 was designed to fulfill a United States military requirement for a long-range photographic reconnaissance fighter. The project progressed with great potential until a disastrous crash of Prototype 1 in the suburbs of Beverly Hills (nearly taking the life of Hughes himself) effectively caused the cancellation of the entire project. The XF-11 would face off with Republic's offering of the XF-12 "Rainbow" only to see neither design chosen at project's end.

The XF-11 was of a traditional twin-boom design, popularized in other forms such as the Northrop P-61 Black Widow and the aforementioned Lockheed P-38 Lightning. The first of two prototypes featured contra-rotating propeller systems on each engine, offering up a great deal of power and performance potential at the cost of increased maintenance and production times. The X-11 featured a powered tricycle landing gear system which proved successful in other designs during the Second world War. The fuselage was constructed of all metal with a two-man crew - the pilot and a radio operator - in a center-fuselage nacelle with complete cabin pressurization for high-altitude capability. Pratt & Whitney brand engines were selected to power the design and these powerplants would turn two four-bladed propeller systems with variable pitch settings. With the Beverly Hills crash blamed on engine failure, the second XF-11 prototype was engineered with traditional non-contra-rotating propeller blade systems.

By all respects, the XF-11 performed admirably well considering the dramatic series of setbacks to the project. Stability and control at high speeds was especially noteworthy though exception was made to the low-altitude stability and performance the system encouraged. A complicated aircraft to fly when compared to others of this type, the XF-11 was nonetheless a capable design in most respects.

Pitted against the Republic XF-12, the XF-11 was deemed as too costly to maintain and produce along with the complications inherent in the system's design. Even with the XF-12 having an edge, the United States Air Force ultimately went with the Boeing produced RB-50 reconnaissance aircraft, citing its respectable range and reconnaissance capabilities equal to that of either XF offering with a lesser price tag.©MilitaryFactory.com
Note: The above text is EXCLUSIVE to the site www.MilitaryFactory.com. It is the product of many hours of research and work made possible with the help of contributors, veterans, insiders, and topic specialists. If you happen upon this text anywhere else on the internet or in print, please let us know at MilitaryFactory AT gmail DOT com so that we may take appropriate action against the offender / offending site and continue to protect this original work.

Specifications



Hughes Aircraft - USA
Manufacturer(s)
United States (cancelled)
Operators National flag of the United States
1946
Service Year
United States
National Origin
Cancelled
Project Status
2
Crew
2
Units


INTELLIGENCE-SURVEILLANCE-RECONNAISSANCE
Surveil ground targets / target areas to assess environmental threat levels, enemy strength, or enemy movement.
X-PLANE
Aircraft developed for the role of prototyping, technology demonstration, or research / data collection.


65.4 ft
(19.94 meters)
Length
101.3 ft
(30.89 meters)
Width/Span
23.2 ft
(7.06 meters)
Height
37,038 lb
(16,800 kilograms)
Empty Weight
58,202 lb
(26,400 kilograms)
Maximum Take-Off Weight
+21,164 lb
(+9,600 kg)
Weight Difference


2 x Pratt & Whitney R-4360-31 radial piston engines developing 3,000 horsepower each.
Propulsion
447 mph
(720 kph | 389 knots)
Max Speed
44,012 ft
(13,415 m | 8 miles)
Ceiling
4,971 miles
(8,000 km | 4,320 nm)
Range


MACH Regime (Sonic)
Sub
Trans
Super
Hyper
HiHyper
ReEntry
RANGES (MPH) Subsonic: <614mph | Transonic: 614-921 | Supersonic: 921-3836 | Hypersonic: 3836-7673 | Hi-Hypersonic: 7673-19180 | Reentry: >19030


None.


XF-11 - Original Series Designation; 2 examples produced with the first offering featuring contra-rotating blades and the second with traditional propeller blade assemblies.
XR-11 - Later Designation


General Assessment
Firepower  
Performance  
Survivability  
Versatility  
Impact  
Values are derrived from a variety of categories related to the design, overall function, and historical influence of this aircraft in aviation history.
Overall Rating
The overall rating takes into account over 60 individual factors related to this aircraft entry.
22
Rating is out of a possible 100 points.
Relative Maximum Speed
Hi: 500mph
Lo: 250mph
This entry's maximum listed speed (447mph).

Graph average of 375 miles-per-hour.
City-to-City Ranges
NYC
 
  LON
LON
 
  PAR
PAR
 
  BER
BER
 
  MOS
MOS
 
  TOK
TOK
 
  SYD
SYD
 
  LAX
LAX
 
  NYC
Operational range when compared to distances between major cities (in KM).
Max Altitude Visualization
Small airplane graphic
Design Balance
The three qualities reflected above are altitude, speed, and range.
Aviation Era Span
Pie graph section
Showcasing era cross-over of this aircraft design.
Unit Production (2)
2
36183
44000
Compared against Ilyushin IL-2 (military) and Cessna 172 (civilian).
>>>>

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Images



1 / 2
Image of the Hughes XR-11 / XF-11
Image from the Public Domain.
2 / 2
Image of the Hughes XR-11 / XF-11
Image from the Public Domain.

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