Jump to content

Canadian Vickers Velos

From Wikipedia, the free encyclopedia

This is the current revision of this page, as edited by AnomieBOT (talk | contribs) at 22:42, 24 September 2022 (Dating maintenance tags: {{Use Canadian English}} {{Use dmy dates}}). The present address (URL) is a permanent link to this version.

(diff) ← Previous revision | Latest revision (diff) | Newer revision → (diff)

Velos
Role Survey floatplane
National origin Canada
Manufacturer Canadian Vickers
First flight 1928
Retired 1928
Status destroyed
Primary user Royal Canadian Air Force
Number built 1

The Canadian Vickers Velos was a Canadian twin-engined float-equipped sesquiplane designed and built by Canadian Vickers Limited in 1928. Designed for survey work, it proved difficult to fly and only one was built.

Operator

[edit]
 Canada

Specification

[edit]
Canadian Vickers Velos 3-view drawing from L'Air June 1,1927

Data from [1]

General characteristics

  • Length: 44 ft 0 in (13.41 m)
  • Wingspan: 68 ft 0 in (20.73 m)
  • Max takeoff weight: 7,918 lb (3,592 kg)
  • Powerplant: 2 × Pratt & Whitney Wasp radial piston engine

Performance

  • Maximum speed: 85 mph (137 km/h, 74 kn)

See also

[edit]

Related lists

References

[edit]
  1. ^ The Illustrated Encyclopedia of Aircraft (Part Work 1982–1985). Orbis Publishing. p. 1040.
[edit]

Media related to Canadian Vickers Velos at Wikimedia Commons