The Sopwith Wallaby was a single-engined long-range biplane built in 1919 by the Sopwith Aviation Company at Kingston upon Thames. It was designed to compete for the Australian government prize of 10,000 pounds for a flight from England to Australia and was powered by a Rolls-Royce Eagle VIII engine, with an open two-seat cockpit whose seats could be retracted inside the enclosed cabin. The aircraft, registered G-EAKS, left Hounslow for Australia on 21 October 1919 and crashed on the island of Bali in the Dutch East Indies on 17 April 1920. It was shipped to Australia, rebuilt as an eight-seat transport and used by Australian Aerial Services.
Facts
Engine Class Top Speed (km/h) Maximum Mass (kg) Comparison
Body StyleAircraft (no road body style) 1 Connections
Exemplifies
Source Sopwith Wallaby (Wikipedia)
Of Make
Source Sopwith Wallaby (Wikipedia)
In the Other Atlases
Manufactured By
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Source Sopwith Wallaby (Wikipedia)Lead, manufacturerQuote, Lead, manufacturer
built during 1919 by Sopwith Aviation Company at Kingston upon Thames
Originated In
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Source Sopwith Wallaby (Wikipedia)Lead, country of originQuote, Lead, country of origin
was a British single-engined long-range biplane
Sources
1. Sopwith Wallaby (Wikipedia)
Lead
built during 1919 by Sopwith Aviation Company
Lead, body style
The Sopwith Wallaby was a British single-engined long-range biplane
Specifications
Rolls-Royce Eagle VIII water cooled V8 engine
Specifications, power
360 hp (270 kW)
Specifications, empty weight
Empty weight: 2,780 lb (1,261 kg)
Specifications, gross weight
Gross weight: 5,200 lb (2,359 kg)
Specifications, speed
Maximum speed: 115 mph (185 km/h, 100 kn)
Lead, manufacturer
built during 1919 by Sopwith Aviation Company at Kingston upon Thames
Lead, country of origin
was a British single-engined long-range biplane
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