Supermarine Scapa
| Scapa | |
|---|---|
 A Supermarine Scapa at the MAEE at Felixstowe, in 1933 | |
| General information | |
| Type | Reconnaissance flying boat, |
| National origin | United Kingdom |
| Manufacturer | Supermarine Aviation Works (Vickers), Ltd. |
| Designer | |
| Primary user | Royal Air Force |
| Number built | 15 |
| History | |
| Introduction date | 1935 |
| First flight | 1932 |
| Retired | 1939 |
| Developed from | Supermarine Southampton |
| Developed into | Supermarine Stranraer |
The Supermarine Scapa was a British general reconnaissance flying boat built by Supermarine that was used by the Royal Air Force between 1935 and 1939. It was developed from the Southampton and formed the basis of the Supermarine Stranraer.
Development
[edit]After experimenting with a three-engine design of flying boat, the Nanok, Supermarine's chief designer R. J. Mitchell decided that the hydrodynamic design developed in the twin-engined Supermarine Southampton, would be suitable for the next aircraft.
A prototype, designated the Southampton IV, was built. It had a hull that exceeded expectations in tests. An Air Ministry Specification was received in November 1931. The test pilot Joseph "Mutt" Summers took first flew the prototype on 8 July, 1932, by which time the name of the type had been changed to Scapa.
After 15 Scapas were built, production was changed to a more powerful development, the Supermarine Stranraer.
Design
[edit]
The Scapa's hull was an all-metal structure, while the wing and tail surfaces had metal structure with fabric covering. The two Rolls-Royce Kestrel V12 engines were mounted in nacelles underslung from the upper wing, and there were two fins, each placed at the mid semi-span of the tailplane. Similar to the Southampton, there were three gun positions: one in the nose, and two staggered in the rear fuselage. Each provided with a single .303 British (7.7 mm) caliber Lewis Mk.I machine guns.
Operators
[edit]
Specifications (Scapa)
[edit]
Data from Supermarine Aircraft Since 1914[1]
General characteristics
- Crew: 5
- Length: 53 ft 0 in (16.15 m) on beaching gear
- Wingspan: 75 ft 0 in (22.86 m)
- Height: 21 ft 0 in (6.40 m) on beaching gear
- Wing area: 1,300 sq ft (120 m2)
- Empty weight: 10,030 lb (4,550 kg)
- Gross weight: 16,080 lb (7,294 kg)
- Powerplant: 2 × Rolls-Royce Kestrel IIIMS V-12 liquid-cooled piston engines, 525 hp (391 kW) each
- Propellers: 2-bladed wooden fixed-pitch propellers
Performance
- Maximum speed: 142 mph (229 km/h, 123 kn) at 3,280 ft (1,000 m)
- Cruise speed: 100 mph (160 km/h, 87 kn) at 5,000 ft (1,524 m)
- Alighting speed: 64 mph (56 kn; 103 km/h)
- Range: 1,000 mi (1,600 km, 870 nmi) with 2,650 lb (1,202 kg) military load
- Service ceiling: 15,500 ft (4,700 m)
- Rate of climb: 625 ft/min (3.18 m/s)
- Time to altitude: 9,840 ft (2,999 m) in 20 minutes
- Wing loading: 12.3 lb/sq ft (60 kg/m2) [citation needed]
- Power/mass: 0.065 hp/lb (0.107 kW/kg)[citation needed]
Armament
- Guns: 3 × 0.303 in (7.7 mm) Lewis guns, one in bow and two amidships
- Bombs: 1,000 lb (454 kg) bombload under the wings
See also
[edit]Related development
Aircraft of comparable role, configuration, and era
Related lists
References
[edit]- ^ Andrews & Morgan 1981, pp. 128.
Sources
[edit]- Andrews, C. F.; Morgan, Eric B. (1981). Supermarine Aircraft since 1914. London: Putnam. ISBN 978-03701-0-018-0.
Further reading
[edit]
- Hillman, Jo·; Higgs, Colin (2020). Supermarine Southampton: The Flying Boat that Made R. J. Mitchell. Barnsley, UK: Pen & Sword Books Limited. ISBN 978-15267-8-497-1.
- Shelton, John (2008). Schneider Trophy to Spitfire: The Design Career of R. J. Mitchell. Sparkford: Hayes Publishing. ISBN 978-1-84425-530-6.
