Westland Wapiti

From Wikipedia, the free encyclopedia

Westland Wapiti
Type general purpose
Manufacturer Westland
Designed by Arthur Davenport
Maiden flight March 1927
Primary users RAF
IAF, RCAF, AAF

The Westland Wapiti was a British general purpose military single engined biplane of the 1920s built by Westland Aircraft Works to a specification for a replacement of the DH9a in RAF service.

It first flew on 7 March 1927.

It was used in Iraq and India, and by Australia and Canada. With the latter it saw service at the start of the Second World War.

Contents

[edit] Service

[edit] Variants

All built by Westland at Yeovil

  • Wapiti I
Two-seat general-purpose biplane for the RAF. Powered by a 420-hp (313-kW) Bristol Jupiter IV radial piston engine. 56 built.
  • Wapiti IA
Improved version for the RAF and RAAF. Powered by a 480-hp (358-kw) Bristol Jupiter IIIF radial piston engine.
  • Wapiti IB
Four exported to South Africa.
  • Wapiti II
440
  • Wapiti IIA
  • Wapiti III:
Two-seat general-purpose biplane for the SAAF. 27 were built under licence in South Africa.
  • Wapiti V:
37
  • Wapiti VI:
Two-seat training version for the RAF. 16 built.
  • Wapiti VII
  • Wapiti VIII:
Two-seat general-purpose biplane for China. Four built.

[edit] Specifications (Wapiti IIA)

Data from The British Bomber since 1914[1]

General characteristics

  • Crew: 2
  • Length: 31 ft 8in (9.65 m)
  • Wingspan: 46 ft 5 in (14.15 m)
  • Height: 13 ft (3.96 m)
  • Wing area: 488 ft² (45 m²)
  • Empty weight: 3810 lb (1732 kg)
  • Loaded weight: 5410 lb (2459 kg)
  • Useful load: lb (kg)
  • Max takeoff weight: lb (kg)
  • Powerplant:Bristol Jupiter VI Radial, 420 hp (313 kW)

Performance

Armament

[edit] Reference

  1. ^ Mason, Francis K (1994). The British Bomber since 1914. London: Putnam Aeronautical Books. ISBN ISBN 0 85177 861 5. 
  2. ^ Thetford, Owen (1957). Aircraft of the Royal Aircraft 1918-57, 1st edition, London: Putnam. 


[edit] External links