| Evolved by the Podlaska Wytwornia Samolotow (Podlasian
Aeroplane Plant), or P.W.S., to meet an official requirement
for a fast two-seat reconnaissance fighter,
the P.W.S.1 parasol monoplane was designed by a team
led by Stanislaw Cywiriski and first flown on 25 April
1927. Of wooden construction apart from a steel-tube
forward fuselage, the P.W.S.1 was powered by a 450hp
Lorraine-Dietrich LD 12Eb 12-cylinder water-cooled
engine and carried an armament of two fixed synchronised
7.7mm guns and two similar-calibre weapons on
a Scarff mount in the rear cockpit. In the latter half of
1927, the aircraft was extensively re-designed and rebuilt
as the P.W.S.1bis, flight testing being resumed
early in 1928. The P.W.S.1bis featured an entirely new
wing and new vertical tail surfaces, empty weight
being reduced marginally but performance remaining
virtually unchanged. As the aircraft held little promise of any major improvement over existing Lotnictwo Wojskowe
equipment, further development was discontinued.
| A three-view drawing (1280 x 858) |
MODEL | P.W.S. 1bis |
WEIGHTS |
Take-off weight | 1950 kg | 4299 lb |
Empty weight | 1375 kg | 3031 lb |
DIMENSIONS |
Wingspan | 13.70 m | 45 ft 11 in |
Length | 8.70 m | 29 ft 7 in |
Height | 3.30 m | 11 ft 10 in |
Wing area | 30.00 m2 | 322.92 sq ft |
PERFORMANCE |
Max. speed | 232 km/h | 144 mph |
Range | 750 km | 466 miles |
vasilli, e-mail, 17.07.2008 19:49 can i have master plan detil...thanks reply |
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