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Bristol Scout F

From Alfawiki
Bristol Aeroplane Company
IndustryAerospace
Founded1910; 116 years ago (1910)
FounderFrank Barnwell
Headquarters
Bristol
,
United Kingdom

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The Bristol Scout E and F represented British single-seat biplane fighters developed in 1916 to accommodate newer, more potent engines. Initially equipped with the Sunbeam Arab, the third prototype served as a platform for testing the Cosmos Mercury engine, marking the beginning of Roy Fedden's collaboration with the Bristol Aeroplane Company. The conclusion of the Armistice halted any further production prospects.

Development

File:Bristol Scout F threequarters.png

By late 1916, there was a notable scarcity of adequately powerful engines suitable for single-seat fighters required to achieve air superiority. Among the limited options was the Hispano-Suiza 8, which suffered from reliability issues and was largely allocated to power the newly introduced Royal Aircraft Factory S.E.5A.[1] In response, Frank Barnwell at the Bristol Aeroplane Company designed a single-seat biplane, designated Scout E, intended to be powered by a proposed 200 hp (150 kW) ten-cylinder water-cooled radial engine developed by Harry Ricardo and Frank Halford. However, this engine did not come to fruition, prompting a search for an alternative power source. The company secured an Air Ministry contract for six units and anticipated receiving 200 hp (150 kW) Hispano-Suiza V8 engines, but by June 1917 these were substituted with 200 hp (150 kW) Sunbeam Arab V8s. Consequently, the design was updated and reclassified as the Scout F.[2]

The Scout F[2] featured a single-bay biplane configuration with staggered wings of unequal span, having straight edges and rounded tips. Ailerons were installed solely on the upper wings, while both upper and lower wings incorporated smooth cutouts to enhance visibility from the open cockpit situated just behind the trailing edge. The tail assembly followed conventional design principles with unbalanced control surfaces. The undercarriage consisted of a fuselage-mounted single-axle main gear positioned ahead of the lower wing, complemented by a tailskid. The water-cooled V-8 Arab engine enabled a streamlined and relatively compact installation, driving a two-blade propeller fitted with a conical spinner. A small bulge atop the cowling housed the coolant header tank, while the radiator was integrated within a tunnel fairing located between the undercarriage legs, equipped with dual shutters to regulate coolant temperature.[2]

Persistent vibration issues plagued the Arab engine, leading to its use being limited to only the first two Scout Fs; the initial prototype took flight in March 1918. This variant achieved a top speed of 138 mph (222 km/h) at sea level and could ascend to 10,000 ft (3,050 m) within 9.5 minutes. The second aircraft was flown by seasoned pilots at the Central Flying School, including Oliver Stuart, who regarded it as possessing superior aerobatic capabilities compared to the SE5a.[2]

File:Bristol Scout F (Mercury).png
Cosmos Mercury-powered Bristol Scout F

Subsequently, Barnwell was approached by Roy Fedden from Cosmos Engineering, located in Fishponds near Bristol. Fedden sought an appropriate airframe to evaluate his 315 hp (235 kW) Cosmos Mercury radial engine under development, leading to the third Scout F being fitted with this powerplant.[2] This installation featured a low-drag cowling with exposed cylinder heads, resulting in an aircraft approximately 10 in (250 mm) shorter than those powered by the Arab engine. The weight increased by 60 lb (27 kg) due to this modification. This version was designated as the Scout F.1 and made its maiden flight on 6 September 1918. Enhanced power output yielded a marginally higher maximum speed alongside a significantly improved climb rate.[2]

The third Scout F was ultimately the final model to fly, although a fourth airframe was constructed as a spare. The end of hostilities brought about cancellation of remaining Mercury contracts, termination of two outstanding Scout F units, and abandonment of plans for mass production.[2]

Specifications (Mercury-powered Bristol Scout F)

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References

Notes

  1. ↑ Barnes 1970, pp. 130–1
  2. ↑ 2.0 2.1 2.2 2.3 2.4 2.5 2.6 Barnes 1970, pp. 130–3

Bibliography

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