The Sopwith T.1 Cuckoo was a British biplane torpedo bomber used by the Royal Naval Air Service (RNAS), and its successor organization, the Royal Air Force (RAF). The T.1 was the first landplane specifically designed for carrier operations, but it was completed too late for service in the First World War. After the Armistice, the T.1 was named the Cuckoo.
|National origin||United Kingdom|
|Manufacturer||Sopwith Aviation Company|
|First flight||June 1917|
|Primary user||Royal Air Force|
Design and developmentEdit
In October 1916, Commodore Murray Sueter, the Air Department's Superintendent of Aircraft Construction, solicited Sopwith for a single-seat aircraft capable of carrying a 1,000 lb torpedo and sufficient fuel to provide an endurance of four hours. The resulting aircraft, designated T.1 by Sopwith, was a large, three-bay biplane. Because the T.1 was designed to operate from carrier decks, its wings were hinged to fold backwards. The T.1 could take off from a carrier deck in four seconds, but it was not capable of making a carrier landing and no arresting gear was fitted. A split-axle undercarriage allowed the aircraft to carry a 1,000 lb Mk. IX torpedo beneath the fuselage.
The prototype T.1 first flew in June 1917, powered by a 200 hp Hispano-Suiza 8Ba engine. Official trials commenced in July 1917 and the Admiralty issued production orders for 100 aircraft in August. Contractors Fairfield Engineering and Pegler & Company had no experience as aircraft manufacturers, however, resulting in substantial production delays. Moreover, the S.E.5a had priority for the limited supplies of the Hispano-Suiza 8. Redesign of the T.1 airframe to accommodate the heavier Sunbeam Arab incurred further delays.
In February 1918, the Admiralty issued a production order to Blackburn Aircraft, an experienced aircraft manufacturer. Blackburn delivered its first T.1 in May 1918. The aircraft immediately experienced undercarriage and tailskid failures, requiring redesign of those components. The T.1 also required an enlarged rudder and offset vertical stabilizer to combat its tendency to swing to the right. Fairfield and Pegler finally began production in August and October, respectively.
A total of 300 T.1s were ordered, but only 90 aircraft had been delivered by the Armistice. A total of 232 aircraft had been completed by the time production ended in 1919. Blackburn Aircraft produced 162 aircraft, while Fairfield Engineering completed 50 and Pegler & Company completed another 20. After the Armistice, many T.1s were delivered directly to storage depots at Renfrew and Newcastle.
After undergoing service trials at RAF East Fortune, the T.1 was recommended for squadron service. Deliveries to the Torpedo Aeroplane School at East Fortune commenced in early August 1918. Training took place in the Firth of Forth, where Cuckoos launched practice torpedoes at targets towed by destroyers. Cuckoos of No. 185 Squadron embarked on HMS Argus in November 1918, but hostilities ended before the aircraft could conduct any combat operations.
In service, the aircraft was generally popular with pilots because the airframe was strong and water landings were safe. The T.1 was easy to control and was fully aerobatic without a torpedo payload. The Arab engine proved unsatisfactory, however, and approximately 20 T.1s were converted to use Wolseley Viper engines. These aircraft, later designated Cuckoo Mk. II, could be distinguished by the Viper's lower thrust line. The Arab-engined variant was designated Cuckoo Mk. I.
Throughout 1917, Commodore Sueter proposed plans for an aerial torpedo attack on the German High Seas Fleet at its base in Germany. The carriers HMS Argus, HMS Furious, and HMS Campania, and the converted cruisers HMS Courageous and HMS Glorious, would have launched 100 Cuckoos from the North Sea. In September 1917, Admiral Sir David Beatty, commander of the Grand Fleet, proposed a similar plan involving 120 Cuckoos launched from eight converted merchant vessels.
Today, no complete Cuckoo airframe survives, but a set of Cuckoo Mk. I wings are preserved at the National Museum of Flight in Scotland.
- Cuckoo Mk. I
- Main production variant. Powered by a 200 hp (149 kW) Sunbeam Arab engine.
- Cuckoo Mk. II
- Mk. I converted to use a 200 hp (149 kW) Wolseley Viper engine.
- Cuckoo Mk. III
- Prototype powered by a 275 hp (205 kW) Rolls-Royce Falcon III engine.
- Sopwith B.1
- Single-seat bomber powered by a 200 hp (149 kW) Hispano-Suiza 8 engine. Two prototypes built.
- Imperial Japanese Navy Air Service - Operated six Cuckoo Mk. II aircraft.
- Royal Naval Air Service
- Royal Air Force
- No. 185 Squadron RAF - Used Cuckoo from October 1918 but was disbanded the following year.
- No. 186 Squadron RAF - Used Cuckoo from late 1918. Was renamed No. 210 Squadron in 1920.
- No. 210 Squadron RAF - Formed in 1920 from No. 186 Squadron, and continued to use the Cuckoo until 1 April 1923 when the unit disbanded.
Specifications (Mk. I)Edit
Data from British Naval Aircraft Since 1912
- Crew: one, pilot
- Length: 28 ft 6 in (8.68 m)
- Wingspan: 46 ft 9 in (14.25 m)
- Height: 10 ft 8 in (3.25 m)
- Wing area: 566 sq ft (52.6 m²)
- Empty weight: 2,199 lb (997 kg)
- Loaded weight: 3,883 lb (1,761kg)
- Powerplant: 1 × Sunbeam Arab V8 engine, 200 hp (149 kW)
- Maximum speed: 105.5 mph (92 kn, 171 km/h)
- Range: 291 nmi (335 mi, 539 km)
- Service ceiling: 12,100 ft (3,688 m)
- 1× 18 inch Mk.IX torpedo
- Davis 1999, p. 123.
- Robertson 1970, p. 125.
- Davis 1999, p. 122.
- Robertson 1970, p. 127.
|Wikimedia Commons has media related to Sopwith Cuckoo.|
- Bruce, J.M. Sopwith B.1 & T.1 Cuckoo: Windsock Datafile 90. Berkhamsted, Hertfordshire, UK: Albatros Publications, 2001. ISBN 1-902207-41-6.
- Davis, Mick. Sopwith Aircraft. Ramsbury, Marlborough, Wiltshire: Crowood Press, 1999. ISBN 1-86126-217-5.
- Layman, R.D. Naval Aviation In The First World War: Its Impact And Influence. London: Caxton, 2002. ISBN 1-84067-314-1.
- Robertson, Bruce. Sopwith – The Man and His Aircraft. London: Harleyford, 1970. ISBN 0-900435-15-1.
- Thetford, Owen. British Naval Aircraft Since 1912. London: Putnam, 1994. ISBN 0-85177-861-5.