Short Seaford

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S.45 Seaford
Seaford NJ205 at Rochester, July 1946
Role Flying boat
National origin United Kingdom
Manufacturer Short Brothers
First flight 30 August 1944
Primary user Royal Air Force
Number built 10
Developed from Short Sunderland
Variants Short Solent

The Short S.45 Seaford was a 1940s flying boat, designed as a long range maritime patrol bomber for RAF Coastal Command. It was developed from the

Short S.25 Sunderland
, and initially ordered as "Sunderland Mark IV".

Background

In 1942, the Air Ministry issued

Specification R.8/42 for a replacement of the Sunderland, as a long range patrol bomber for service in the Pacific Ocean. It required more powerful engines, better defensive armament, and other enhancements.[1][2]

Design and development

The Sunderland Mark IV used major structural elements of the Sunderland Mark III, with a fuselage stretch of 3 ft ahead of the wing, an extended and redesigned planing bottom, the same wing with thicker Duralumin skinning, and

Bristol B.17 dorsal turret, twin .50 in (12.7 mm) guns in a Glenn-Martin tail turret, and another .50 in (12.7 mm) machine gun in a hand-held waist position on each side of the fuselage. The turrets were all electrically powered. Two prototypes and thirty production aircraft were ordered as the Sunderland Mark IV.[1][2]

Operational history

On 30 August 1944, the prototype (MZ269) first flew from the

BOAC as G-AGWU, then returned to MAEE as NJ201 in February 1946. In April 1946, the other six production Seafords were delivered to No. 201 Squadron RAF for brief operational trials. In 1948, those six aircraft were modified as civilian airliners at Belfast, then leased to BOAC with the designation Solent 3.[5]

Operators

 United Kingdom

Specifications (S.45 Seaford)

Data from Green 1968, p. 107[6]

General characteristics

  • Crew: 8–11 (two pilots, radio operator, navigator, engineer, bomb-aimer, three to five gunners)
  • Length: 88 ft 6+34 in (26.994 m)
  • Wingspan: 112 ft 9+12 in (34.379 m)
  • Height: 37 ft 3 in (11.35 m)
  • Wing area: 1,687 sq ft (156.7 m2)
  • Empty weight: 45,000 lb (20,412 kg)
  • Gross weight: 75,000 lb (34,019 kg)
  • Powerplant: 4 × Bristol Hercules XIX 14-cylinder radial engines, 1,720 hp (1,280 kW) each

Performance

  • Maximum speed: 242 mph (389 km/h, 210 kn) at 500 ft (150 m)
  • Cruise speed: 155 mph (249 km/h, 135 kn) at 5,000 ft (1,500 m)
  • Range: 3,100 mi (5,000 km, 2,700 nmi) [7][8]
  • Service ceiling: 14,000 ft (4,300 m)
  • Rate of climb: 880 ft/min (4.5 m/s)
  • Time to altitude: 18 min to 10,000 ft (3,000 m)

Armament

Survivor

Short S.45 Seaford NJ203, converted to a Short Solent in 1948, is displayed at the Oakland Aviation Museum, Oakland, California.[9][10]

See also

Aircraft of comparable role, configuration, and era

Related lists

Notes

  1. ^ a b Barnes 1989, pp. 357
  2. ^ a b Green 1968, p. 106.
  3. ^ Barnes 1967, p. 360.
  4. ^ London 2003, p. 196.
  5. ^ Barnes 1989, pp. 360–363
  6. ^ Green 1968, p. 107.
  7. ^ Barnes 1967, p. 368.
  8. ^ London 2003, pp. 264–265.
  9. ^ Ogden (2007)
  10. ^ ""Short Solent"". Archived from the original on 19 June 2016. Retrieved 14 March 2015.

Bibliography

External links

  • Short Seaford Flight 3 January 1946 (3 pages of diagrams and images)