The Siddeley-Deasy Sinaia, also known as the Armstrong Whitworth Sinaia, was a large twin-engined biplane day bomber designed to meet an Air Ministry requirement. It was the third and last design of the team led by John Lloyd and F. M. Green at Siddeley-Deasy before the firm was rebadged by merger as the Sir W. G. Armstrong Aircraft Company, a change that had already taken effect when it first flew on 25 June 1921. Its most unusual feature was the defensive armament: the engines sat in nacelles on top of the lower wings, and each nacelle was extended rearwards and upwards to carry a gunner's cockpit with a gun ring, so that two gunners could cover both sides, with a third position in the slanted nose. It was powered by two 500 hp Siddeley Tiger water-cooled V-12 engines, a little-tested design that proved unreliable and interrupted the flight trials. Two examples were ordered but only one was completed, and by October 1921 structural problems had appeared and it was taken out of use.
Facts
Maximum Mass (kg) EngineTwo Siddeley Tiger water-cooled V12 engines of 500 hp each 1 Connections
Exemplifies
Source Siddeley-Deasy Sinaia (Wikipedia)
Of Make
Source Siddeley-Deasy Sinaia (Wikipedia)
In the Other Atlases
Manufactured By
Also in Business Atlas: the manufacturer of this subject.
Source Siddeley-Deasy Sinaia (Wikipedia)Lead, alternative nameQuote, Lead, alternative name
also known as the Armstrong Whitworth Sinaia
Originated In
Also in Geography Atlas: where this subject originated.
Source Siddeley-Deasy Sinaia (Wikipedia)Development, requirementQuote, Development, requirement
It was designed to meet an Air Ministry requirement for a day bomber
Sources
1. Siddeley-Deasy Sinaia (Wikipedia)
Development, first flight
which flew for the first time on 25 June 1921
Lead, type
was a twin-engined biplane day bomber
Development, end of trials
the only Sinaia ever built was taken out of use
Lead, number completed
Two examples were ordered by the Air Ministry but only one was completed
Specifications, gross weight
Gross weight: 16,000 lb (7,257 kg)
Specifications, powerplant
Powerplant: 2 × Siddeley Tiger water-cooled V12 engines, 500 hp (370 kW) each
Lead, alternative name
also known as the Armstrong Whitworth Sinaia
Development, requirement
It was designed to meet an Air Ministry requirement for a day bomber
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