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Westland N.1B

TheWestland N.1B was a prototypeBritish single-enginedfloatplanefighter aircraft of theFirst World War. The first aircraft to be designed byWestland Aircraft, it was a single-enginedtractorbiplane. Despite good performance, only two aircraft were built, theRoyal Naval Air Service operating landplane fighters from ships instead.

N.1B
RoleFighter
National originUnited Kingdom
ManufacturerWestland Aircraft
First flightAugust 1917
StatusPrototype
Number built2

Development and design

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In 1916, theBritish Admiralty drew up Requirement N.1B for a single-seat floatplane orflying boat fighter aircraft to operate from theRoyal Navy'sseaplane carriers, demanding a speed of 110 mph (177 km/h) and a ceiling of 20,000 ft (6,100 m). Three companies submitted designs in response,Blackburn andSupermarine with flying boats (theBlackburn N.1B andSupermarine Baby), while Westland proposed a floatplane, theWestland N.1B. Westland received an order for two aircraft.[1]

Westland's design, which was the first original design built by Westland, was a single-engined tractorbiplane of wooden construction.[1] It had a deep fuselage, while its two-bay wings were designed to fold to save space on ship, and were fitted with trailing-edgeflaps. It was powered by a single Bentley A.R.1rotary engine (later known as theBR1) and carried a singlesynchronised forward-firingVickers machine gun on the nose, and aLewis gun firing over the upper wing.[2][3] The first N.1B was fitted with 11 ft (3.35 m) longSopwith main floats and a 5 ft (1.52 m) long tail float, while the second N.1B had much longer (17 ft 6 in 5.34 m) main floats, which removed the need for a tail float.[4]

The first N.1B,serial numberN16 was first flown byHarry Hawker from Westland'sYeovil factory in August 1917.[5] The two N.1Bs were evaluated at thePort Victoria Marine Experimental Aircraft Depot in October 1917,[6] demonstrating good performance and handling.[5] By this time, however, theRoyal Naval Air Service was operatingSopwith Pup landplanes from flying-off platforms aboard ships, which did not require the carrier to heave-to in order to lower a seaplane to the water, and was planning to carry out similar operations with theSopwith Camel, and the N.1B programme was cancelled.[6]

Specifications (Second prototype)

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Data from Westland Aircraft since 1915[7]

General characteristics

  • Crew: 1
  • Length: 26 ft5+12 in (8.065 m)
  • Wingspan:31 ft3+12 in (9.538 m)
  • Height: 11 ft 2 in (3.40 m)
  • Wing area: 278 sq ft (25.8 m2)
  • Empty weight: 1,513 lb (686 kg)
  • Gross weight: 1,987 lb (901 kg)
  • Powerplant: 1 ×Bentley BR.1 9-cylinder air-cooled rotary piston engine, 150 hp (110 kW)
  • Propellers: 2-bladed fixed-pitch propeller

Performance

  • Maximum speed: 107 mph (172 km/h, 93 kn)
  • Endurance: 2 hours 45 minutes[6]
  • Service ceiling: 10,400 ft (3,200 m)[6]
  • Time to altitude: 5,000 ft (1,500 m) in 10 minutes

Armament

See also

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Aircraft of comparable role, configuration, and era

References

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  1. ^abJames 1991, p.69.
  2. ^Mason 1992, p.117.
  3. ^Bruce 1957, p.705.
  4. ^James 1991, pp.70–71.
  5. ^abJames 1991, p.71.
  6. ^abcdBruce 1957, p. 707.
  7. ^James 1991, pp.72–73.
  • Bruce, J.M.British Aeroplanes 1914–18. London:Putnam, 1957.
  • James, Derek N.Westland Aircraft since 1915. London:Putnam, 1991.ISBN 0-85177-847-X.
  • Mason, Francis K.The British Fighter since 1912. Annapolis, USA:Naval Institute Press, 1992.ISBN 1-55750-082-7.

External links

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