STATUS: Retired, Out-of-Service
MANUFACTURER(S): Armstrong Whitworth - United Kingdom
OPERATORS: United Kingdom
LENGTH: 22.24 feet (6.78 meters)
WIDTH: 27.89 feet (8.5 meters)
HEIGHT: 11.48 feet (3.5 meters)
WEIGHT (EMPTY): 1,246 pounds (565 kilograms)
WEIGHT (MTOW): 2,039 pounds (925 kilograms)
ENGINE: 1 x Clerget 9Z rotary engine of 110 horsepower driving two-bladed propeller at nose.
SPEED (MAX): 84 miles-per-hour (135 kilometers-per-hour; 73 knots)
RANGE: 211 miles (340 kilometers; 184 nautical miles)
CEILING: 9,843 feet (3,000 meters; 1.86 miles)
RATE-OF-CLIMB: 455 feet-per-minute (139 meters-per-minute)
Detailing the development and operational history of the Armstrong Whitworth F.K.9 Quadruplane Reconnaissance Fighter Prototype.
Entry last updated on 1/12/2018.
Authored by Staff Writer. Content ©www.MilitaryFactory.com.
There proved plenty of experimentation with multi-winged aircraft designs during World War 1 (1914-1918). The biplane was more or less the standardized fighter/bomber form while some monoplane fighters did go on to see considerable time in the air. Triplanes managed a short, though useful, revolution but quickly fell out of favor. Beyond these categories was the "quadruplane" - four-winged arrangement intended to harness the agility and control offered from use of four parallel planes in the wing structure, this providing for exceptional lifting and turning properties, qualities critical to close-in dogfights. Several firms of the period experimented with such types but many fell by the wayside as being much too impractical for military service.
Armstrong Whitworth of Britain tried its hand at a quadruplane in the form of the FK.9. It was a two-seat, single-engine form intended for reconnaissance and fighter duties. Development was through private venture in the hopes of interesting the Royal Flying Corps on the design. Its offshoot, the FK.10, would become one of the few quadruplane designs of the war to be adopted form formal service.
First-flight of a prototype FK.9 was had in the summer of 1916 and changes were instituted to remedy several issues: the engine cowling was completely reworked and the tail fin given greater surface area. All-new wings were added and these carried larger-area ailerons as well. The undercarriage track was made wider for improved ground running. Power was served from a Clerget 9Z rotary engine of 110 horsepower driving a simple, two-bladed wooden propeller in the nose. The crew of two sat in tandem across two open-air cockpits, these positioned aft of the four horizontal planes cranked forward. Standard armament was 1 x .303 Vickers machine gun in a fixed, forward-firing emplacement operated by the pilot and 1 x .303 Lewis Gun managed from a trainable mounting by the rear gunner / observer.
The FK.9 was officially evaluated at the Central Flying School during November and into December of 1916. It proved worthy enough to warrant a serial production contract for fifty aircraft - though improvements to the design necessitated the change in designation to "FK.10" for these mounts.
A single FK.9 aircraft was built followed by just 8 x FK.10 - the 50-strong order never fulfilled due to the design's heavy drag. None saw combat service in the whole of the war.
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Relative Maximum Speed Rating
This entry's maximum listed speed (84mph).
Graph average of 75 miles-per-hour.
Graph showcases the Armstrong Whitworth F.K.9's operational range (on internal fuel) when compared to distances between major cities.
Useful in showcasing the era cross-over of particular aircraft/aerospace designs.
Unit Production Comparison
Comm. Market HI*: 44,000 units
Military Market HI**: 36,183 units