Supermarine Southampton
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Southampton | |
---|---|
Type | Military Flying Boat |
Manufacturer | Supermarine |
Maiden flight | 10 March 1925 |
Primary users | Royal Air Force Argentina Australia Japan |
Number built | 83 |
Variants | Scapa StranraerStranraer |
The Supermarine Southampton was one of the most successful flying boats of the between-war period. It was a development of the Supermarine Swan, which was used for a 10 passenger service between England and France.
Contents |
[edit] History
The Southampton was designed by the team of RJ. Mitchell, better known as the designer of the Spitfire. Because of the success of the Swan, the Air Ministry ordered six Southamptons direct from the drawing board, which was very unusual. As the Swan had acted in effect as a prototype, development time was short. The first flight of a production aircraft was made on 10 March 1925, and delivery to the RAF started in the middle of 1925. Further aircraft were sold to a number of other countries. Eight were sold to the Argentine, while Turkey & Australia brought one aircraft each. Japan also purched a single aircraft which was later converved into an 18 passenger cabin airliner. One aircraft was placed on the British Civil Register (G-AASH) and was operated by Imperial Airways. In all 83 Southamptons were constructed. This does not include the single Southampton MK X which had three engines and was a single prototype.
[edit] Description
The Southampton was a two-engine biplane flying boat. The Southampton Mk I had both its hull and its wings manufactured from wood. The Southampton Mk II had a hull with a single thickness of metal (the Mk I had a double wooden bottom). This change gave a weight saving of 900 lb (409 kg) allowing for an increase of range of approximately 200 miles (325 km). In 1929 twenty-four of the Mk I were converted by having newly built metal hulls replacing the wooden ones. Some of the later aircraft were built with metal wings and were probably desinated as Mk III. There were three positions for machine guns, one in the nose and two staggered in the rear fuselage.
[edit] Power Plants
Different power plants were fitted as below
- Mk I - Napier Lion V
- Mk II - Napier Lion Va
- Argentine - Lorraine 12E
- Turkey - Hispano-Suiza 12Nbr
- Experimental - Bristol Jupiter IX and Rolls-Royce Kestrel
[edit] Operators
[edit] Military Operators
[edit] Civil Operators
[edit] Specifications (Southampton II)
Data from Supermarine Aircraft since 1914[1]
General characteristics
- Crew: Four
- Length: 49 ft 8½ in (15.15 m)
- Wingspan: 75 ft (22.86 m)
- Height: 20 ft 5 in (6.2 m)
- Wing area: 1,448 ft² (134.5 m²)
- Empty weight: 9,696.5 lb (4,398 kg)
- Loaded weight: 15,200 lb (6,895 kg)
- Useful load: lb (kg)
- Max takeoff weight: lb (kg)
- Powerplant: 2× Napier Lion VA , 500 hp (373 kW) each
Performance
- Never exceed speed: knots (mph, km/h)
- Maximum speed: 83 knots (95 mph, 153 km/h) at sea level
- Cruise speed: knots (mph, km/h)
- Stall speed: knots (mph, km/h)
- Range: 473 nm (544 mi, 876 km) at 86 mph (139 km/h) & 2,000 ft (610 m)
- Service ceiling: 5,950 ft (1,814m)
- Rate of climb: 368 ft/min (1.87 m/s)
- Wing loading: 10.50 lb/ft² (51.26 kg/m²)
- Power/mass: 0.066 hp/lb (0.11 kW/kg)
- Climb to 6000 ft (1829 m) 29 minutes 42 seconds
- Endurance 6.3 hours
Armament
- Three Lewis guns, one in bows and two amidships.
- 1,100 lb of bombs under the wings.
[edit] Reference
- ^ Andrews, CF; Morgan, EB (1987). Supermarine Aircraft since 1914, 2nd edition (in English), London: Putnam. ISBN 0 85177 800 3.
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