| Conceived by Emile Dewoitine to participate in the 1921
C1 (single-seat fighter) programme, the D 1 high-wing
monoplane was of advanced structural concept. It
mated fabric-covered metal wings with an oval-section
metal fuselage covered by duralumin sheet. Armament
consisted of two 7.7mm synchronised Vickers guns
and power was provided by a 300hp Hispano-Suiza
8Fb (HS 42) eight-cylinder water-cooled engine. The
prototype was flown on 18 November 1922, the principal
criticism being the poor forward visibility for the
pilot. A 120mm pylon was therefore inserted between wing and fuselage, the fighter, now referred
to as the D 1bis, thus becoming a parasol monoplane.
This modification was effected in August 1923, by
which time the first three (of 10) pre-series aircraft had
been supplied for official evaluation in the initial configuration.
Two of these were lost in accidents and the
third was modified to D 1bis parasol form. The next five
pre-series. aircraft (the fourth, fifth and sixth having
been ordered by Czechoslovakia, Japan and Italy respectively,
and the seventh and eighth by Switzerland)
were all completed to D 1bis standard, but continuing
criticism of forward view led to replacement of the shallow
pylon between wing and fuselage by a cabane of
inverted-vee struts on the prototype which thus became
the D 1ter. The two pre-series aircraft for Switzerland
were modified to this standard prior to delivery, the two lost during official trials) were completed as D 1ter fighters, the cabane struts being standardised for
production D 1s. A contract had been placed in November
1923 on behalf of the Aeronautique Navale for 44 D 1s, with the government providing guarantees for 150
aircraft. The production contract was placed with the
SECM (Societe d'Emboutissage et de Constructions
Mecaniques) which flew its first series D 1 on 18
January 1925. Sixty (later reduced to 44) were ordered
by Yugoslavia, and after the D 1 was selected by Italy in
preference to the Dornier Do H Falke, licence manufacture
(with modifications) was undertaken as the
Ansaldo A.C.2. The Aeronautique Navale
took delivery of its D 1s from early 1925, and in the previous
year an order for 20 had been placed on behalf of
the Forces Aeriennes Terrestres, although these were
never to equip a service unit.
 | A three-view drawing (640 x 442) |
WEIGHTS |
Take-off weight | 1240 kg | 2734 lb |
Empty weight | 820 kg | 1808 lb |
DIMENSIONS |
Wingspan | 11.50 m | 38 ft 9 in |
Length | 7.50 m | 25 ft 7 in |
Height | 2.75 m | 9 ft 0 in |
Wing area | 20.00 m2 | 215.28 sq ft |
PERFORMANCE |
Max. speed | 250 km/h | 155 mph |
Range | 400 km | 249 miles |
Do you have any comments?
|
|  COMPANY PROFILE All the World's Rotorcraft
|