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Hansa-Brandenburg W.23

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W.23
General information
TypeFlying-boat fighter
ManufacturerHansa und Brandenburgische Flugzeug-Werke
Designer
Number built3
History
First flight1917

TheHansa-Brandenburg W.23 was aprototypebiplaneflying-boat fighter designed by theHansa-Brandenburg Aircraft Company (Hansa Brandenburgische Flugzeugwerke) for theImperial German Navy's (Kaiserliche Marine) Naval Air Service (Marine-Fliegerabteilung) duringWorld War I. Three aircraft were ordered in 1917 and delivered the following year, but it was not ordered into production.

Design and development

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The W.23 was the culmination of the company's line ofpusher configuration flying-boatbiplane fighters reaching back to 1916'sCC, all of which had aswept lower wing, wingfloats, and a single-stephull to allow the aircraft to break free from the water more easily. It greatly resembled the precedingW.18, but its hull was longer and it had a water-cooled 160-metric-horsepower (118 kW)Mercedes D.IIIstraight-six engine that drove a two-bladed, fixed-pitchpropeller. The aircraft's armament consisted of a 7.92-millimeter (0.312 in)LMG 08/15 and a20-millimeter (0.79 in) Beckerautocannon, both mounted in the upper deck of the nose.[1][2]

Three prototypes were ordered in June 1917 and were delivered to the Seaplane Experimental Command (Seeflugzeug-Versuchs-Kommando) in June 1918.[3] Details are scanty, but aviation historians William Green and Gordon Swanborough state that the W.23's flight characteristics were so poor that the program was cancelled.[4] Two aircraft were located atSeddin when theAllies inspected the German seaplane bases in December 1918. Their ultimate fate is unknown, but it is likely that they werescrapped.[5]

Specifications

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Data from Hansa-Brandenburg Aircraft of WWI: Volume 2–Biplane Seaplanes. Great War Aviation Centennial Series[6]

General characteristics

  • Crew: 1
  • Length: 9.13 m (29 ft 11 in) overall
  • Upper wingspan: 10.7 m (35 ft 1 in)
  • Lower wingspan: 10.24 m (33 ft 7 in)
  • Height: 3.6 m (11 ft 10 in)
  • Wing area: 34.7 m2 (374 sq ft)
  • Empty weight: 918 kg (2,024 lb)
  • Gross weight: 1,261 kg (2,780 lb)
  • Powerplant: 1 ×Mercedes D.III water-cooledstraight-six engine, 120 kW (160 hp)
  • Propellers: 2-bladed fixed-pitch propeller

Performance

  • Maximum speed: 165 km/h (103 mph, 89 kn)
  • Service ceiling: 3,000 m (9,800 ft)
  • Time to altitude:
  • 800 m (2,600 ft) in 6 minutes
  • 1,000 m (3,300 ft) in 7 minutes
  • 1,500 m (4,900 ft) in 12 minutes
  • 2,000 m (6,600 ft) in 18 minutes 12 seconds
  • 3,000 m (9,800 ft) in 38 minutes 18 seconds

Armament

See also

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Related lists

References

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  1. ^Owers, p. 83
  2. ^Green & Swanborough, pp. 85–86
  3. ^Owers, pp. 6-7
  4. ^Green & Swanborough, p. 86
  5. ^Andersson & Sanger, p. 22
  6. ^Owers, p. 86

Bibliography

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  • Andersson, Lennart & Sanger, Ray (2014).Retribution and Recovery: German Aircraft and Aviation 1919 to 1922. Air-Britain (Historians).ISBN 978-0-85130-467-0.
  • Green, William & Swanborough, Gordon (2001) [1994].The Complete Book of Fighters: An Illustrated Encyclopedia of Every Fighter Built and Flown (Revised and Updated ed.). Salamander Books.ISBN 1-84065-269-1.
  • Owers, Colin A. (2015).Hansa-Brandenburg Aircraft of WWI: Volume 2–Biplane Seaplanes. Great War Aviation Centennial Series. Vol. 18. n.p.: Aeronaut Books.ISBN 978-1-935881-32-2.
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