Supermarine S.6

The Supermarine S.6 (later designated the S.6A) is a 1920s British single-engined single-seat racing seaplane built by Supermarine and designed by its chief designer, R.J. Mitchell, who refined the earlier Supermarine S.5 to produce a larger, more powerful aircraft. Two aircraft, ''N247'' and ''N248'', were built to participate in the 1929 Schneider Trophy contest. Rolls-Royce produced the R engine for the new all-metal aircraft. The engine's initial issues—such as the short time between overhauls and the heat generated when the engine power was increased to —were resolved within a few months before the aircraft were completed at Supermarine’s works at Woolston, Southampton.

The day before the 1929 race, one of ''N247''s pistons was discovered to be faulty; the piston was replaced during the night. The race on the following day was won by the British team, with ''N247'' coming first at a speed of , whilst ''N248'' set World closed-circuit records for . For the 1931 race, the S.6 was redesigned as the Supermarine S.6B, to take a more powerful version of the R engine. The two existing S.6s were brought up to a similar standard as the S.6Bs, but ''N247'' was destroyed prior to the contest during a fatal accident. The S.Bs were retired after the 1931 contest. The surviving S.6A is on display at the Solent Sky museum in Southampton.

Design and development

Following the success of the Supermarine S.5 in the 1927 Schneider Trophy contest. Supermarine's chief designer R.J. Mitchell designed its successor, the Supermarine S.6, to Specification 8/28. Refining the design of the earlier S.5, Mitchell designed a larger all-metal aircraft. The metal-framed wings of the S.6 were designed to be made using aluminium, so as to assist in reducing the overall weight of the aircraft. To achieve the required lift, the wings were made to be longer than those of the lighter S.5.

The aircraft industry during the First World War had used up nearly all the world supply of seasoned spruce, a requirement for wooden aeroplanes at that time, and so the ability to produce metal-built aircraft for any future conflict was deemed by the British government to be essential.

An innovation by Mitchell was the use of duralumin radiators on the surface of the wings. Made both to withstand forces that tended to cause the wings to twist, and to minimise air resistance, they were made of two thicknesses of metal that allowed water to pass between them.

Rolls-Royce R engine

As the Napier Lion VIIB engine was judged by Supermarine to be incapable of further development, in February 1929, the British Government signalled to Rolls-Royce that they could proceed with producing the R engine for Supermarine. The engine, an adaptation of the Rolls-Royce Buzzard, was designed and manufactured by 4 May, but this machine was found to overheat after 15 minutes. By the middle of July, many of the engine's initial problems had been resolved, but the valves were still causing problems. The time between overhauls was able to be lengthened to five hours when the fuel was diluted, and the engine power was able to be increased to at a frequency of 3,000 rpm. The engine needed of petrol to complete a race, as it consumed fuel at a rate of . By July 1928, Mitchell had been given drawings of the engine from Rolls-Royce, which he used to work on improving the aerodynamic qualities of the aircraft.

To help alleviate problems of engine cooling caused by the high rate of heat generation, the S.6 had surface radiators built into the floats as well as on the wings. Additional cooling was provided by means of air flowing through the internal structure of the wings. The new engine weighed , a weight that meant that it had to be better supported by moving the float struts forward by a slight amount. The increase in fuel consumption meant that both floats had to incorporate steel fuel tanks.

In February 1929, Supermarine was authorised to build two machines for the 1929 contest. The aircraft (with designated serial numbers ''N247'' and ''N248'') were built together at their works at Woolston, Southampton.

Operational history

The two S.6s were delivered to Calshot in August 1929 for operation by the RAF High Speed Flight. ''N247'' first flew on 10 August, and ''N248'' a fortnight later. Soon after ''N247'' arrived at Calshot, it was found that one of the floats was so low in the water on take-off that it made the aircraft rotate on the surface. Ripples were sufficient to enable ''N247'' to become airborne. An issue with overheating was sorted by installing extra radiators.

When a British entrant, a Gloster VI was forced by engine trouble to be withdrawn, the only two British entrants that remained were the S.6s, and so the S.5 (N219) was prepared for the contest. During a final check of ''N247'', a speck of metal was discovered on a spark plug, which revealed a faulty piston. It was forbidden for the entire engine to be replaced once it was installed, but components could be changed prior to the race. The engine block was changed during the night—by specialist Rolls-Royce engineers from a party who happened to have come down to Southampton from Derby to watch the race—so that the engine was running smoothly by the start of the next day.

The 1929 Schneider Trophy race took place off the English coast north of the Isle of Wight, under ideal weather conditions, and with at least a million people assembled along the beaches to witness the event. ''N247'', piloted by Flying Officer H.R.D. Waghorn, came first at a speed of . ''N248'' was disqualified when it turned inside one of the marker poles, but nonetheless, set World closed-circuit records for during its run. Following the victory, the British Prime Minister Ramsay MacDonald publicly pledged official support for the 1931 contest, a decision that was later reversed by the government.

For the 1931 Schneider Trophy race, also to be held at Calshot, the S.6 was adapted to take a more powerful version of the R engine. Two new aircraft, designated the Supermarine S.6B, were built. The two existing S.6s, now designated as S.6As, were provided with new floats, additional cooling areas and statically-balanced control surfaces. All four aircraft were brought up to a similar standard. During the initial flight of the improved ''N247'' on 2 June, the pilot experience dangerous levels of tail flutter (a form of resonance), which was only alleviated when masses were fixed to the rudder.

The British plan for the 1931 contest was to fly one of the S.6Bs, ''S1595'', around the course alone, with ''N248'' in reserve. If both ''S1595'' and ''N248'' failed in their attempts, ''N247'' would be used. However, ''N247'', flown by Navy Lieutenant G.N. Brinton, was destroyed in a fatal takeoff accident during a pre-contest training exercise. ''N248'' remained as part of the team but did not fly in the race. ''S1595'' went on to win a race in which only British aircraft participated.

Aircraft on display

''N248'' was used in the 1942 British biographical film about Mitchell, ''The First of the Few''. Until the 1960s, the aircraft was displayed incorrectly as S.6B ''S1596'' as a visitor attraction in a building adjacent to the Royal Pier, Southampton. The S.6A was restored from 1983 onwards, and repainted in its original 1931 scheme. It can be seen on display at the Solent Sky museum in Southampton.

Operators

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* Royal Air Force
** High Speed Flight

Specifications (N247)

See also

Notes

References

Citations

Sources

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Further reading

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External links

* Silent news reels (
Transport – Aviation: Supermarine Schneider Cup Plane (1929)
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To Keep That Schneider Cup (1929)
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357+ Miles an Hour (aka 357.7 Miles per Hour) (1929)
from British Pathe

Article
from ''Popular Mechanics'' about the S.6 and the 1929 Schneider Cup contest, based on
December 1929 edition of the magazine

{{Supermarine aircraft

Schneider Trophy
1920s British sport aircraft
Floatplanes
S.6
Low-wing aircraft
Single-engined tractor aircraft
Aircraft first flown in 1929
Single-engined piston aircraft