Canadian Vickers Velos
From Infogalactic: the planetary knowledge core
| Canadian Vickers Velos | |
|---|---|
| 300px | |
| Role | Survey floatplane |
| National origin | Canada |
| Manufacturer | Canadian Vickers |
| First flight | 1928 |
| Introduction | 1928 |
| Retired | 1928 |
| Status | destroyed |
| Primary user | Royal Canadian Air Force |
| Number built | 1 |
The Canadian Vickers Velos was a 1927 Canadian twin-engined float-equipped sesquiplane designed and built by Canadian Vickers Limited. Designed for survey work, it proved difficult to fly and only one was built.
Operator
Specification
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
- Related lists
References
 |
Wikimedia Commons has media related to Canadian Vickers military aircraft. |
- Notes
- ↑ Orbis 1985, p. 1040
- Bibliography
- Lua error in package.lua at line 80: module 'strict' not found.
