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.

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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

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Specifications

Service Year

1946

Origin

United States

Status

CANCELLED
Development Ended.

Crew

2

Production

2
UNITS

Hughes Aircraft - USA

(View other Aviaton-Related Manufacturers)

United States (cancelled)

(OPERATORS list includes past, present, and future operators when applicable)

✓ Intelligence-Surveillance-Reconnaissance (ISR), Scout
Surveil ground targets / target areas to assess environmental threat levels, enemy strength, or enemy movement.

✓ X-Plane (Developmental, Prototype, Technology Demonstrator)
Aircraft developed for the role of prototyping, technology demonstration, or research / data collection.

Length

65.4 ft
(19.94 m)

Width/Span

101.3 ft
(30.89 m)

Height

23.2 ft
(7.06 m)

Empty Wgt

37,038 lb
(16,800 kg)

MTOW

58,202 lb
(26,400 kg)

Wgt Diff

+21,164 lb
(+9,600 kg)

(Showcased structural values pertain to the base Hughes XR-11 / XF-11 production variant)

Installed: 2 x Pratt & Whitney R-4360-31 radial piston engines developing 3,000 horsepower each.

Max Speed

447 mph
(720 kph | 389 kts)

Ceiling

44,012 ft
(13,415 m | 8 mi)

Range

4,971 mi
(8,000 km | 14,816 nm)

♦ MACH Regime (Sonic)

Sub

Trans

Super

Hyper

HiHyper

ReEntry

♦

(Showcased performance specifications pertain to the base Hughes XR-11 / XF-11 production variant. Performance specifications showcased above are subject to environmental factors as well as aircraft configuration. Estimates are made when Real Data not available. Compare this aircraft entry against any other in our database or View aircraft by powerplant type)

None.

Supported Types

(Not all ordnance types may be represented in the showcase above)

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

PAR

BER

MOS

TOK

SYD

LAX

NYC

Hughes XR-11 / XF-11 operational range when compared to distances between major cities (in KM).

Max Altitude Visualization

Design Balance

The three qualities reflected above are altitude, speed, and range.

Aviation Era Span

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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