| The SPAD (Societe pour l'Aviation et ses Derives) concern,
although headed by Louis Bleriot, operated as a
separate organisation from the Societe Bleriot-Aeronautique
until 1921, when SPAD was absorbed and the
subsequent progeny of its design team became officially
known by the title of Bleriot SPAD. The first
fighter in the SPAD line to receive the Bleriot SPAD
appellation was the Bleriot SPAD 41, designed by
Andre Herbemont and essentially a single-seat derivative
of the SPAD S.XX two-seater of 1918. Powered by a
300hp Hispano-Suiza HS 8Fb eight-cylinder water-cooled
engine with two individual Lamblin radiators in
place of the familiar circular frontal radiator, the Bleriot
SPAD 41 was a staggered single-bay biplane with a
sweptback upper wing and unswept lower wing. It
featured a wooden monocoque fuselage. The prototype
was flown for the first time at Buc on 17 July 1922, but
official evaluation revealed an inadequate service ceiling
and no production was ordered, the aircraft subsequently
being modified for racing.
 | A three-view drawing (1685 x 1230) |
MODEL | S.41 |
CREW | 1 |
ENGINE | 1 x 300hp Hispano-Suiza 8Fb |
WEIGHTS |
Take-off weight | 1307 kg | 2881 lb |
Empty weight | 887 kg | 1956 lb |
DIMENSIONS |
Wingspan | 8.68 m | 29 ft 6 in |
Length | 6.65 m | 22 ft 10 in |
Height | 2.76 m | 9 ft 1 in |
Wing area | 26.40 m2 | 284.17 sq ft |
PERFORMANCE |
Max. speed | 238 km/h | 148 mph |
Cruise speed | 205 km/h | 127 mph |
Ceiling | 6850 m | 22450 ft |
ARMAMENT | 2 x 7.7mm |
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