Vickers Viking

From Wikipedia, the free encyclopedia

Vickers Viking
Vickers Viking IV of the Royal Canadian Air Force, 1926
Type amphibian
Manufacturer Vickers
Maiden flight 1919
Produced 1919-1923

The Vickers 54 Viking was a single-engined amphibious aircraft designed for military use shortly after World War I.

Research on Vickers' second amphibious aircraft type began in December 1918 with tests of alternative fuselage/hull designs occurring in an experimental tank at St Albans in Hertfordshire, England. A prototype, registered G-EAOV, was a 5-seat cabin biplane with a pusher propeller driven by a Rolls-Royce motor. Sir John Alcock died taking this aircraft or another early example to the Paris exhibition on 18 December 1919, whilst trying to land at Cote d'Everard, near Rouen, Normandy in foggy weather.

The next example, G-EASC, known as the Viking II, had a greater wing span and a 360 hp Rolls-Royce Eagle VIII motor. The Viking III machine, piloted by Captain Cockerell, won first prize in the amphibian class in Air Ministry competitions held in September and October, 1920. The Viking IV incorporated further refinements and had a wider cabin above a hull one foot wider, an example being G-EBBZ in which Ross Smith and J.M. Bennett (partners in the 1919 England to Australia flight) died on 13 April 1922 just outside the Brooklands racetrack near Weybridge in Surrey. Most of these Mark IV Vikings had a Napier Lion engine.

The last Viking amphibians were built during 1923, but the name was re-used for the twin-piston engined Vickers VC.1 Viking airliner some 22 years later, which saw service as the Valetta with the RAF and other air arms. Some Viking amphibians were built by Canadian Vickers Limited, a subsidiary company in Montreal with no previous plane making experience.

General characteristics

  • Crew: One, pilot
  • Capacity: 2 passengers
  • Length: 34 ft 0 in (10.36 m)
  • Wingspan: 50 ft 0 in (15.24 m)
  • Height: 15 ft 1 in (4.60 m)
  • Wing area: 594 ft² (55.2 m²)
  • Empty weight: 3,750 lb (1,701 kg)
  • Loaded weight: 5,600 lb (2,451 kg)
  • Max takeoff weight: lb (kg)
  • Powerplant:Rolls-Royce Eagle piston engine, 360 hp (269 kW)

Performance

Designation sequence


Advanced Search
Included Web Search Engines


Safe Search

close

Top Matching Results

Occasionally Search.com will highlight specialized results that are based on the context of your query. Examples of specialized results include specific links to news, images, or video.

Top Matching Results may highlight information from other Search.com pages, content from the CNET Network of sites, or third party content. The listings are based purely on relevance. Search.com does not receive payment for listings in this section but our partners that provide this data may get paid for listing these products.

Sponsored Links

This section contains paid listings which have been purchased by companies that want to have their sites appear for specific search terms and related content. These listings are administered, sorted and maintained by a third party and are not endorsed by Search.com.

Search Results

Search.com sends your search query to several search engines at one time and integrates the results into one list which has been sorted by relevance using Search.com's proprietary algorithm. You can customize the list of search engines included in your metasearch from the preferences.

The search engines that are used in your metasearch may allow companies to pay to have their Web sites included within the results. To view the Paid Inclusion policy for a specific search engine, please visit their Web site. Search.com does not accept payment or share revenue with any search engine partner for listings in this section.