| In July 1920, Capt Frank Barnwell and his team began
design work on an all-metal parasol fighter monoplane
intended to be built in both single- and two-seat form,
and three prototypes were ordered. In the event, wood
was used for the wing construction of the prototypes,
the fuselages being of steel tube. By March 1922, when the name Bullfinch was officially adopted, the decision
had been taken to complete two of the prototypes as
single-seaters, these being delivered in April 1923.
Armed with two 7.7mm Vickers machine
guns, the Bullfinch single-seaters were flown experimentally
by the RAF and were found to offer a relatively
good performance on the 425hp of a Bristol Jupiter III
radial, but no production order was forthcoming. The
third prototype was completed as the two-seat Bullfinch
II.
 | A three-view drawing (1278 x 840) |
WEIGHTS |
Take-off weight | 1454 kg | 3206 lb |
Empty weight | 986 kg | 2174 lb |
DIMENSIONS |
Wingspan | 11.71 m | 38 ft 5 in |
Length | 7.44 m | 24 ft 5 in |
Height | 3.27 m | 11 ft 9 in |
Wing area | 24.8 m2 | 266.94 sq ft |
PERFORMANCE |
Max. speed | 217 km/h | 135 mph |
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