Supermarine Sea Lion III

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Sea Lion III
photograph of the Sea Lion III
Henry Biard aboard the Sea Lion III
Role Racing
flying-boat
National origin UK
Manufacturer Supermarine Aviation Works
Designer
R.J. Mitchell
First flight 1923
Retired 1923
Number built 1

The Supermarine Sea Lion III was a British

Reginald Mitchell, it was a modification of Supermarine's Supermarine Sea Lion II. It was powered by a 550 hp (410 kW) Napier Lion
engine.

Sea Lion III was entered for the 1923 Schneider Trophy contest at Cowes. Supermarine's test pilot Henry Biard flew the aircraft and managed third place, reaching a speed of 151.16 mph (243.27 km/h). The performance of the Sea Lion III led to Supermarine designing seaplanes instead of flying boats as racers.

Development

The British aircraft company

Reginald Mitchell,[3] who incorporated a 450 hp (340 kW) Napier Lion engine loaned by Napier.[2][4]

1923 Schneider Trophy race

The course of the 1923 Schneider Trophy race

The Sea Lion II was flown by Henry Biard, who won the race at an average speed of 145.7 mph (234.5 km/h),[2] The victory was the first post-World War I success by a British aircraft in an international competition[5]

For the 1923 Schneider Race, which was held at

Curtiss CR-3 seaplanes, reaching a speed of 151.16 mph (243.27 km/h).[2] Supermarine's managing director Hubert Scott-Paine said after the trophy was won by the Americans:[7]

Our drawing office people got all the speed they possibly could out of the machine. We did the best we could and have no regrets. Sea Lion III was 11 mph faster than Sea Lion II, and the credit for this fine performance was due to several people, one of whom is Mr. R.J. Mitchell, who designed both machines.

The British defeat caused Supermarine to abandon using outclassed flying boats as racers, in favour of seaplanes.[7] The Sea Lion III was transferred to the Royal Air Force in 1923.[2]

Operators

 United Kingdom

Specifications (Sea Lion II)

Data from Supermarine Aircraft since 1914[8]

General characteristics

  • Crew: 1
  • Length: 24 ft 9 in (7.54 m)
  • Wingspan: 32 ft 0 in (9.75 m)
  • Wing area: 384 sq ft (35.7 m2)
  • Empty weight: 2,115 lb (959 kg)
  • Gross weight: 2,850 lb (1,293 kg)
  • Powerplant: 1 ×
    Napier Lion II
    W-12 water-cooled piston engine, 450 hp (340 kW)
  • Propellers: 4-bladed fixed-pitch wooden pusher propeller

Performance

  • Maximum speed: 160 mph (260 km/h, 140 kn)
  • Endurance: 3 hours

See also

Related lists

References

  1. ^ Andrews & Morgan 1987, pp. 5, 60.
  2. ^ a b c d e f g h Jackson 1988, p. 314.
  3. ^ Baker 1994, p. 144.
  4. ^ Andrews & Morgan 1987, p. 60.
  5. ^ Pegram 2016, p. 36.
  6. ^ a b Mitchell 2006, p. 51.
  7. ^ a b Mitchell 2006, p. 53.
  8. ^ Andrews & Morgan 1987, p. 68.

Sources

  • Andrews, C. F.; Morgan, E. B. (1987). Supermarine Aircraft since 1914. London: Putnam. .
  • .
  • Jackson, A. J. (1988). British Civil Aircraft 1919–1972: Volume III. London: Putnam. .
  • Mitchell, Gordon (2006). R.J. Mitchell: Schooldays to Spitfire. Stroud: Tempus. .
  • Pegram, Ralph (2016). Beyond the Spitfire: The Unseen Designs of R.J. Mitchell. Pegram: The History Press. .