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WORLD WAR 1

Armstrong Whitworth F.K.10


Two-Seat Quadruplane Fighter Aircraft (1917)


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Jump-to: Specifications

Just eight out of the 50 Armstrong Whitworth F.K.10 quadruplanes ordered were completed for service with the Royal Flying Corps and Royal Naval Air Service.



Authored By: Staff Writer | Last Edited: 03/17/2021 | Content ©www.MilitaryFactory.com; the following text is exclusive to this site.
The Armstrong Whitworth F.K.10 fighter was the full production-minded realization of the earlier F.K.9 prototype (detailed elsewhere on this site). The types were formed around a single-engine, twin-seat "quadruplane" platform and the F.K.10 model became one of the few quadruplane designs to see formal adoption by a major air service during World War 1 (1914-1918). However, the series managed only eight completed forms before being given up for good. The F.K.9 prototype first-flew in late-1916 and paved the way for the modified (and slightly improved) F.K.10 that followed in 1917.

At this point in the war the biplane was entrenched as the primary fighter standard though a few companies were able to sell the various air services on a monoplane fighter design. The triplane's appearance in 1917 vaulted multi-winged gunnery platforms to the forefront but this dominance was short-lived and the biplane remained the standard. Aeronautical engineers saw the value in adding more wings to an aircraft but this ultimately came at a steep price - drag. Multiple wings provided additional lift and better controlling at the expense of additional air resistance which did not bode well as a strong quality for a fighter to have - speed was still the call of the day as it were. As such, there were many failed experiments in the realm of more-than-three winged aircraft during the war years - the F.K.10 more or less being an exception.

Developed for the reconnaissance-fighter role, the F.K.10 carried a tandem, two-seat crew configuration in which the pilot managed a sole, synchronized and fixed .303 Vickers machine gun at front and the rear gunner / observer was given management of a .303 Lewis Gun set atop a trainable mounting at rear. The fuselage of the aircraft was well-rounded at the front and tapered to the rear with slab-sides running the length. The tail unit was of a traditional single-finned arrangement with elevated horizontal planes positioned along the sides. The engine was held in a compartment at the nose of the aircraft and drove a two-bladed wooden propeller in the usual way. The undercarriage was wheeled and of a "tail-dragger" configuration - the main legs being wheeled for ground running.
The quadruplane wing arrangement appropriately featured four planes set parallel to one another. A thick supporting structure (called an "interplane strut") was run through all four planes for the needed strength. The stacked wings were noticeably cranked forwards from the bottom-up when viewing the aircraft's side profile. The pilot's cockpit was positioned aft of the engine but under the top-most wing plane and behind the second plane. The third plane was positioned midway along the sides of the fuselage with the fourth plane held low and away from the belly of the aircraft.

Power for the series was to come from a Clerget 9B rotary engine of 130 horsepower, giving it more output than the original prototype's Clerget 9Z rotary of 110 horsepower.

Design of the F.K.10 was attributed to Dutchmen Frederick Koolhoven dating back to 1916's F.K.9 prototype. His surname would go on to drive some of the aircraft designs emerging from the Netherlands during the lead-up to World War 2 (1939-1945).

The F.K.9 impressed enough that a production order for 50 aircraft was signed by the Royal Flying Corps (RFC). However the noticeable issue of drag soon limited the need for the quad-winged F.K.10 and only eight were completed in all - the biplane still being the favored wing arrangement for fighters and bombers. Five examples were finished before the formal cancellation of the contract came down though three more followed for the Royal Naval Air Service and saw some testing before the end.

Specifications



Service Year
1917

Origin
United Kingdom national flag graphic
United Kingdom

Status
RETIRED
Not in Service.
Crew
2

Production
8
UNITS


Armstrong Whitworth - United Kingdom
National flag of the United Kingdom United Kingdom
(OPERATORS list includes past, present, and future operators when applicable)
Air-to-Air Combat, Fighter
General ability to actively engage other aircraft of similar form and function, typically through guns, missiles, and/or aerial rockets.
Intelligence-Surveillance-Reconnaissance (ISR), Scout
Surveil ground targets / target areas to assess environmental threat levels, enemy strength, or enemy movement.


Length
22.2 ft
(6.78 m)
Width/Span
27.8 ft
(8.48 m)
Height
11.5 ft
(3.50 m)
Empty Wgt
1,246 lb
(565 kg)
MTOW
2,028 lb
(920 kg)
Wgt Diff
+783 lb
(+355 kg)
(Showcased structural values pertain to the base Armstrong Whitworth F.K.10 production variant)
Installed: 1 x Clerget 9B rotary engine developing 130 horsepower and driving two-bladed wooden propeller at nose.
Max Speed
84 mph
(135 kph | 73 kts)
Ceiling
10,007 ft
(3,050 m | 2 mi)
Range
211 mi
(340 km | 630 nm)
Rate-of-Climb
455 ft/min
(139 m/min)


♦ 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


(Showcased performance specifications pertain to the base Armstrong Whitworth F.K.10 production variant. Compare this aircraft entry against any other in our database. View aircraft by powerplant type)
1 x .303 Vickers machine gun in fixed, forward-firing mounting over the nose, synchronized to fire through the spinning propeller blades.
1 x .303 Lewis Gun on trainable mounting in rear cockpit.


Supported Types


Graphical image of an aircraft medium machine gun


(Not all ordnance types may be represented in the showcase above)
Hardpoint Mountings: 0


F.K.10 - Base Series Designation; eight examples delivered out of 50 ordered.


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