| S.4 | |
|---|---|
.jpg) Official photograph of the S.4, from the magazineFlight in October 1925 | |
| General information | |
| Type | Racingfloatplane |
| National origin | United Kingdom |
| Manufacturer | Supermarine |
| Designer | |
| Status | Destroyed 23 October 1925 |
| Number built | 1 |
| History | |
| First flight | 24 August1925 |
The Supermarine S.4 was a 1920s British single-engined monoplane built by the companySupermarine. Designed by a team led by the company's chief designer, R. J. Mitchell, it was designed to compete in the 1925 Schneider Trophy contest.
Mitchell's design is considered by historians as revolutionary. Built of wood with an unbraced cantilever wing, the S.4 was powered by a Napier Lion engine developed to produce 700 horsepower (520 kW) over a short period. Less than a month after its maiden flight on 24 August 1925, it raised the world's seaplane speed record to 226.752 miles per hour (364.922 km/h).
At Bay Shore Park inBaltimore in the US, the venue of the 1925 contest, the S.4's rear end was damaged by a falling pole during a gale before the event. During navigation trials on 23 October the repaired aircraft was observed to be performing well, but then, for reasons that have not been fully explained, it went out of control, and was destroyed when it dived into the sea from 100 feet (30 m), injuring the pilot,Henry Biard. Mitchell then used his experience gained working on the S.4 to design its successor, the Supermarine S.5.
During 1925, R. J. Mitchell was working on a new aircraft to compete in that year's Schneider Trophy competition.[1] The decision to begin the design process was made jointly byNapier and Supermarine on 18 March 1925.[2] Following the success of the Americans during the previous contest, Mitchell was fully aware of the need to reduce drag to increase speed. Supermarine's new design was for a mid-wingcantilever floatplane which resembled a Frenchmonoplane, theBernard SIMB V.2, which had broken theflight airspeed record in December 1924.[3][4] The new design was in marked contrast to theflying boats Mitchell had designed for previous Schneider Trophy races, which had won in 1922 and come third behind the AmericanCurtiss CR seaplanes in 1923.[5]
The designationS.4 was given by Mitchell,[3] "S" standing forSchneider.[6] He regarded the three previous Schneider Trophy entrants (theSupermarine Sea Lion series) as S.1, S.2, and S.3.[2] The S.4 was the first Schneider Trophy entrant to be supported by the British government, who agreed to buy the aircraft if Supermarine and Napier covered the initial costs of development and construction.[7] TheAir Ministry provided the British teams with greater freedom than was given by the U.S. government to their designers.[3]
The S.4 was a monoplane seaplane with an unbracedcantilever wing and semi-monocoquefuselage, powered by a specially developed version of theNapier Lion,[8] developed to produce 700 horsepower (520 kW) over a short period.[9] The aircraft was primarily constructed from wood: the single-piece unbraced wing had twospars withspruce flanges andplywood webs, and was covered with plywood braced bystringers.[8] The fuselage had a covering of diagonally laid spruce planking over plywood formers constructed around a pair of steelA-frames,[8] to which the engine bearers and wing spars were attached and which carried the floats.[10] The single-step floats were metal.[11] The S.4 lacked the newly designedsurface radiators, at that time still unavailable, but it was aerodynamic and also judged to beaesthetically pleasing.[3]
In September 1925, the magazineFlight reported:[12]
Perhaps one may describe the Supermarine-Napier S.4 as having the appearance of having been designed in an inspired moment, but having all that is considered best in British construction incorporated in its details. That the design is bold, no one will deny, and we think the greatest credit is due to Mr. R. J. Mitchell, chief designer of the Supermarine Aviation Works, for his courage in breaking away from stereotyped methods and striking out on entirely novel lines.
Allocated the civil registration G-EBLP and the Air Ministryserial number N197,[13][14] the S.4 first flew on 24 August 1925, witnessed by Mitchell, who went out in a motorboat withLord Mountbatten.[2][15] Testing took place atCalshot, because of the long take-off runs that were required.[3]
Supermarine's chief test pilotHenry Biard was reportedly unhappy with the S.4, disliking theunbraced wings and the cockpit position, which was well back behind the wings. The location of the cockpit was potentially hazardous, as it restricted the pilot's view ahead, particularly during take-off and landing. On its maiden flight, the S.4 came close to colliding with anocean liner because of this.[16][note 1]
On 13 September 1925, on a 1.864-mile (3.0 km) straight course overSouthampton Water,[15] the S.4 raised the world's seaplane speed record (and the British speed record) to 226.752 miles per hour (364.922 km/h),[16][13] which created a sensation in the press when it was announced a month later.[3][16]
With high hopes of a British victory in the forthcoming Schneider Trophy competition atBay Shore Park,Baltimore, the S.4, together with twoGloster III biplanes, was shipped to the U.S. aboard theSSMinnewaska, free of charge.[17][18] During the voyage, Supermarine's pilot Biard slipped playingtennis, and injured his wrist.[18]
Bad weather meant that those Schneider Trophy competitors that had already arrived for the competition had little opportunity to practise the course.[19] The aircraft were forced to remain in their crates while canvashangars were being erected on the beach to accommodate them.[18] Biard caughtinfluenza, but recovered sufficiently to participate in the competition. The windy conditions had, however, blown down the hangar where the S.4 was being kept, and the rear end of the aircraft had been damaged by a falling pole. The S.4 was repaired in time to take part in navigation trials on 23 October 1925.[19]
During the trials, the S.4 initially performed well but, upon its return to shore, thecontrol column began to oscillate violently and Biard lost control of the machine at high speed.[19] The S.4 was seen to stall, before falling flat into the sea from 100 feet (30 m). Biard, who initially had lost consciousness when he was still strapped into the aeroplane, was able to resurface from the sea bed, and cling to some floating wreckage.[20][21] The firstlaunch sent out to him broke down with engine trouble, and he had to be rescued by a second launch. Mitchell, who was on board the boat that rescued Biard, jokingly asked the injured man: "Is the water warm?"[22] Biard was later found to have broken two ribs.[20]
Parts of the wrecked aircraft weresalvaged by the sloopHMS Valerian, which had been dispatched to Baltimore from theBermuda to support the British team.[23][24][21][25] Most sources have suggested the accident was due toflutter,[26] but although an enquiry was later held,[21] the reasons for the crash were never clearly established.[27]
The race was won two days later byLieutenantJames Doolittle, flying aCurtiss R3C at an average speed of 232.573 mph (374.443 km/h), which was faster than the S.4's world record of a month before.[26] It was evident to the other national teams that the American approach towards the contest—which involved training for the pilots and development testing of the aircraft—was required. Mitchell was to say as much when he gave a lecture to theRoyal Aeronautical Society in 1927. From 1925 onwards, the Air Ministry developed a policy of usingwind tunnel tests to analyse the performance of the high-speed aircraft they produced.[20]
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The Supermarine S.4 was a revolutionary aircraft that was years ahead of its time, and which "set the pattern in specific aircraft design that persisted through the [1930s and 1940s]".[28] It was designed with new technology, with floats that were the most advanced of their time, and a wing, with its lack of external bracing wires, that had never before been incorporated into a Supermarine aircraft. The aviation historianJohn D. Anderson notes that the aircraft "represented Mitchell's willingness to incorporate new technology within the framework of a tried and tested intellectual methodology for conceptual design", and was "a revolution in airplane design" that "influenced all subsequent Schneider racers".[29] The winning aircraft of the 1926 Schneider contest, the ItalianMacchi M.39, was distinctly similar to the S.4.[30] Mitchell used the practical experience gained when he designed its successor, theSupermarine S.5.[31] The S.4 has been described as "his first outstanding success".[32]
Drawings and archival footage of the plane's construction, and five minutes of film that show the aircraft's first takeoff and flight, are preserved inLeslie Howard's biographical film about Mitchell,The First of the Few (1942).[33]
The S.5's design included features intended to reduce the wing flutter considered at the time to have contributed to the loss of the S.4; the monoplane wings were braced with wires.[34] The S.5 was given a smaller fuselagecross section and more streamlined floats, modifications designed to produce increases in speed over its predecessor. The greatest speed increase—considered to be approximately 24 miles per hour (39 km/h)—was produced by the introduction of surface radiators to cool the engine, as they significantly reduced the drag forces acting on the aircraft.[30] Tests made on a model of the S.4 at theNational Physics Laboratory which were done after the crash revealed that the Lamblin radiators accounted for a third of the aircraft's drag and that without them the S.4 would have been the "cleanest" monoplane in the world.[35]
Data from Supermarine Aircraft since 1914[36]
General characteristics
Performance
