| A contender to Specification 0.22/26 calling for a high-speed
shipboard reconnaissance-fighter capable of
being flown with either wheel or float undercarriage and suitable for catapult operation from cruisers and
larger warships, the S.10 Gurnard was awarded a two-prototype
contract. One of the prototypes, the Gurnard
I, was to be powered by a 525hp Bristol Jupiter X nine-cylinder
air-cooled radial engine, and the other, the
Gurnard II, was to have a 525hp Rolls-Royce Kestrel IIS
water-cooled 12-cylinder Vee-type engine. A single-bay
biplane of metal construction with fabric skinning,
the Gurnard had an armament of one fixed forward-firing
7.7mm machine gun and a similar-calibre
weapon on a Scarff ring for the second crew
member. The Gurnard II was the first to fly, on 16 April
1929, as a floatplane, the Gurnard I following in landplane
form three weeks later, on 8 May. Both prototypes
were tested at the A&AEE, but the Hawker
Osprey was selected in preference and no production of
the Gurnard was ordered. The Gurnard II was flown -
commencing on 15 June 1931 - as an amphibian with a
single main float.
 | A three-view drawing (1280 x 868) |
MODEL | Gurnard II |
WEIGHTS |
Take-off weight | 2360 kg | 5203 lb |
Empty weight | 1662 kg | 3664 lb |
DIMENSIONS |
Wingspan | 11.27 m | 37 ft 0 in |
Length | 9.60 m | 32 ft 6 in |
Wing area | 39.85 m2 | 428.94 sq ft |
PERFORMANCE |
Max. speed | 258 km/h | 160 mph |
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