Saunders-Roe SR.A/1
1947
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Saunders-Roe SR.A/1

Conceived as a means of applying the promised advantages of jet propulsion to a single-seat fighter flying boat for use in the Pacific, the SR.44 was proposed by Saunders-Roe (Saro) during 1943. This proposal led to a contract for three prototypes being placed in May 1944 to Specification E.6/44. To be designated SR.A/1 before first flight, the fighter was of light alloy construction throughout, power being provided by two Metropolitan Vickers F2/4 Beryl turbojets and provision being made for an armament of four 20mm cannon grouped in the forward hull above the air intake. The first SR.A/1 did not fly until 16 July 1947, its Beryl turbojets each being rated at 1465kg. The second flew on 30 April 1948 with 1587kg Beryls and the third followed on 17 August of that year with fully rated Beryls of 1746kg. As no operational requirement remained for a fighter flying boat, official interest waned, and, after a brief revival of interest during the Korean War, the last surviving SR.A/1 was retired in June 1951.

Saunders-Roe SR.A/1


Specification 
 MODELSR.A/1
 CREW1
 ENGINE2 x Metropolitan-Vickers F2/4 Beryl turbojets, 1474-1746kg
 WEIGHTS
    Take-off weight8633 kg19033 lb
    Empty weight5108 kg11261 lb
 DIMENSIONS
    Wingspan14.02 m45 ft 12 in
    Length15.24 m50 ft 0 in
    Height5.11 m16 ft 9 in
    Wing area38.60 m2415.49 sq ft
 PERFORMANCE
    Max. speed824 km/h512 mph

3-View 
Saunders-Roe SR.A/1A three-view drawing (1685 x 1120)


Sgt.KAR98, 27.12.2007
What was the size of this plane?
Corsairoz, trevsastar(@)hotmail.com, 04.12.2007
The last remaining SRA-1 is still in perfect condition and survives in Solentsky Museum in Southampton UK.

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FACTS AND FIGURES

© The axial-flow Beryl engine was chosen because two of them could be mounted side-by-side in a relatively narrow fuselage.

© The position of the small cockpit enclosure on the fuselage meant that the pilot's view ahead disappeared during the take-off run.

© The possibility of water ingestion into the nose-mounted intake was the reason for its high position in the nose.



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