Short Shetland

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S.35 Shetland

Type	reconnaisance flying-boat
Manufacturer	Short Brothers
Maiden flight	14 December 1944
Number built	2

The Short Shetland was a British high-speed, long-range, 4-engined flying-boat built by Short Brothers at Rochester, Kent. It was designed to meet an Air Ministry requirement (defined in Specification R.14/40) for a very-long range reconnaissance flying boat. The design used the company's experience with large scale production of the Short Sunderland.

1 Design and development
- 1.1 Short S.35 Shetland I
- 1.2 Short S.40 Shetland II
2 Specifications (S.35)
3 References
4 External links
5 Related content

[edit] Design and development

Specification R.14/40 replaced an earlier specification R.5/39 which was an up-armed revision of specification R.3/38 for for a faster flying boat than the Short Sunderland. Shorts, among others, had tendered a design for R.5/39 but the Ministry had changed their minds about the need for an immediate replacement for the Sunderland. R.5/39 had considered a maximum weight up to 84,000 lb - R14/40 allowed for a maximum takeoff of nearly 100,000 lb (45 tonnes) with a bomb load of 20,000 lb. The projected engines were the Bristol Centaurus radial or the Napier Sabre inline.

Shorts and the other British manufacturer of big flying boats, Saunders-Roe (Saro), were involved in the competitive tender for R.14/40; Saro proposed the Saunders-Roe S.41. Rather than selecting either company's design, the Air Ministry asked the companies to submit a combined project, stipulating the terms under which the work was to be shared between them. The detailed design was performed by Saro, their experience with the "Shrimp" contributing to the hull shape, as well as building the wing. Shorts built the hull and tail and did the final assembly.

[edit] Short S.35 Shetland I

The first prototype and to be the only Shetland I (Serial Number DX166) first flew on 14 December 1944. The aircraft flew without gun turrets and was delivered to the Marine Aircraft Experimental Establishment (MAEE) at Felixstowe in October 1945. Testing indicated satisfactory water handling but the stabilising floats were mounted too low and did not offer sufficient clearance for takeoffs with maximum load. ^[1]Flight testing revealed problems with the harmonization of controls and marginal longitudinal stability. Before the trials were complete, the aircraft burnt out at its moorings on 28 January 1946 as a result of a galley fire.

[edit] Short S.40 Shetland II

With the end of the war, the second prototype (Serial Number DX171) was completed as a civil transport and designated Shetland II. It was designed to carry 70 passengers but only 40 seats were fitted. Registered "G-AGVD," the Shetland II's first flight took place on 17 September 1947. After trials, it was delivered to Short's factory at Belfast, but no orders were forthcoming and it performed only limited flight trials before being scrapped in 1951.

[edit] Specifications (S.35)

General characteristics

Crew: 11
Capacity: 70
Length: 110 ft (33.5 m)
Wingspan: 150 ft 4 in (46.75 m)
Height: 38 ft 8in (11.7 m)
Wing area: 2,636 ft² (244.9 m²)
Empty weight: 75,860 lb (34,410 kg)
Loaded weight: 120,000 lb (54,431 kg)
Max takeoff weight: 125,000 lb (56,700 kg)
Powerplant: 4× Bristol Centaurus VII radial piston, 2,500 hp () each

Performance

Maximum speed: 263 mph at 6,500 ft (424 km/h)
Range: 4,410 miles (3,835 nm) (7,100 km)
Service ceiling: 17,000 ft (5,180 m)

Armament

(as planned)

Three turrets (two 0.5 in Browning machine guns: nose, mid-upper and tail positions)
Up to 4000 lb (1814 kg) of bombs or depth charges

[edit] References

^ Green 1962, p.110.

Buttler, Tony. British Secret Projects: Fighters & Bombers, 1935-1950. Hinckley, UK: Midland Publishing Ltd., 2004. ISBN 1-85780-179-2.
Green, William. Flying Boats: Vol.5 (Warplanes of the Second World War). London: Macdonald & Co., 1962.
Jackson, A.J. British Civil Aircraft since 1919, Volume 2 (2nd Edition). London: Putnam, 1973. ISBN 0-370-10010-7.