| The shortcomings in handling qualities and manoeuvrability
demonstrated by the P.W.S.10 prototypes led its
designers, Grzedzielski and Bobek-Zdaniewski, in 1930
to develop a biplane version, the P.W.S.15, as a private
venture for comparative testing. One of the two
P.W.S.10 prototypes was fitted with a modestly staggered
unequal-span single-bay biplane cellule with
N-type interplane struts. Retaining the engine and
armament of the P.W.S.10, the P.W.S.15 lacked the
shortcomings of the parasol monoplane, possessing a
superior climb rate and an essentially similar maximum
speed. However, while the P.W.S.15 was under test, the
company received a production contract for the
P.W.S.10, and, rather than risk its cancellation in favour
of the biplane with consequent production disruption,
dismantled the prototype biplane without submitting it
to official flight test.
MODEL | ÐWS-15 |
CREW | 2 |
ENGINE | 1 x 450hp Lorraine-Dietrich LD 12Eb |
WEIGHTS |
Take-off weight | 1515 kg | 3340 lb |
Empty weight | 1145 kg | 2524 lb |
DIMENSIONS |
Wingspan | 10.00 m | 33 ft 10 in |
Length | 7.50 m | 25 ft 7 in |
Height | 3.00 m | 10 ft 10 in |
Wing area | 23.00 m2 | 247.57 sq ft |
PERFORMANCE |
Max. speed | 250 km/h | 155 mph |
Cruise speed | 215 km/h | 134 mph |
Ceiling | 6500 m | 21350 ft |
Rate of climb | 390 m/min | 1300 ft/min |
Range | 520 km | 323 miles |
ARMAMENT | 2 x 7.7mm |
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