Canadian Vickers Vanessa
{{Infobox aircraft
|name=Vanessa
|image=Canadian Vickers Vanessa ExCC.jpg
|type=transport seaplane
|manufacturer=Canadian Vickers
|designer=
|first_flight=
|status=Cancelled
|primary_user=Royal Canadian Air Force (intended)
|number_built=1
}}
The Canadian Vickers Vanessa was a Canadian biplane transport floatplane of the 1920s evaluated by the Royal Canadian Air Force (RCAF) and used briefly for delivering air-mail.
Design and development
The Vanessa was developed as a private venture commercial seaplane.
It was a single-engine, twin-float cabin biplane of mixed construction. The enclosed cabin fuselage was constructed of steel tubing as were various support structures along with the tail surfaces. The wings were of wood construction and the entire aircraft was fabric covered. Its interplane struts were unusual in forming a pair of "X"s on each side, when viewed from the front which eliminated the need for wire bracing and improved access to the cabin. Ailerons were fitted to each of the equal span wings which were linked with connecting rods. As first built, these ran the full span of the wings, but were reduced to about half the span shortly afterwards.
Testing
One prototype, registered G-CYZJ, was built, after which the Royal Canadian Air Force indicated an interest in the type as a communications aircraft. Testing indicated that the aircraft was under-powered and the {{cvt|200|hp}} Armstrong Siddeley Lynx was replaced with a {{cvt|220|hp}} Wright Whirlwind.
In September 1927, the Vanessa was used for several airmail flights.{{citation needed|date=November 2011}} On 9 September 1927 at Rimouski, Quebec on the Saint Laurence River about {{cvt|280|km}} east of Quebec City, its RCAF pilot received {{cvt|502|lb}} of mail from the west-bound RMS Empress of France. While taxiing for takeoff, a wake from a passing vessel hit it, breaking a strut, which then allowed the aircraft's starboard float to be hit by the propeller, which sliced the float in half. The aircraft capsized, broke up, and sank but the pilot escaped and the mail was recovered, which continued on by rail.
The wreck was salvaged but was found to be uneconomical to repair and development was abandoned.
Despite a very brief career, the Vanessa has the distinction of being one of the first enclosed cabin aircraft designed in Canada.
Specifications (Vanessa–Lynx engine)
File:Canadian_Vickers_Vanessa_3-view_L'Air_July_1,1927.png
{{Aircraft specs
|ref=Jane's all the World's Aircraft 1928,{{cite book |title=Jane's all the World's Aircraft 1928 |editor1-last=Grey |editor1-first=C.G. |year=1928 |publisher=Sampson Low, Marston & company, ltd |location=London |pages=71c–72c}} RCAF.com{{cite web|url=http://www.rcaf.com/aircraft/misc/vanessa/index.php?name=Vanessa|title=RCAF.com|access-date=9 April 2012|publisher=RCAF.com}}
|prime units?=imp
|crew=1
|capacity=4 passengers
|length m=9.13
|span m=10.7
|height m=3.73
|wing area sqft=410
|airfoil=
|empty weight lb=2120
|gross weight lb=
|max takeoff weight lb=3400
|fuel capacity={{cvt|400|lb}}
|more general=
|eng1 number=1|eng1 name=Armstrong Siddeley Lynx|eng1 type=7-cylinder air-cooled radial piston engine|eng1 hp=200
|prop blade number=2|prop name=fixed-pitch wood propeller
|prop dia m=|prop dia ft=|prop dia in=|prop dia note=
|max speed mph=103
|max speed note=
- Landing speed:' {{cvt|45|mph|kn km/h}}
|cruise speed mph=
|stall speed mph=
|range miles=
|ceiling ft=12000
|climb rate ftmin=550
|wing loading lb/sqft=
|power/mass=
}}
References
{{reflist}}
Bibliography
- {{cite book|last1=Molson|first1=K.M.|last2=Taylor|first2=H.A.|title=Canadian aircraft since 1909|date=1982|publisher=Canada's Wings|location=Stittsville, Ont.|isbn=0-920002-11-0|edition=1. publ.}}
{{commons category|Canadian Vickers Vanessa}}
{{Canadian Vickers aircraft}}
{{Aircraft manufactured in Canada}}
Category:1920s Canadian civil utility aircraft