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PWS-10 & PWS-15

The PWS-10 was a Polish fighter aircraft.

First work on a domestic fighter to replace ill-fated French SPAD 61s in the Polish Air Force was initiated by PWS in 1927.

The main designers were Aleksander Grzędzielski and Augustyn Zdaniewski.

In 1929 the prototype was built, and it first flew in March 1930.

At the same time, the more modern fighter PZL P.1 was developed by the PZL.

Despite the P.1 being a more capable fighter, the War Ministry decided that it needed further work, and a series of 80 PWS-10 was ordered as a temporary measure.

In comparison with the advanced P.1, the PWS-10 was a more classic design, a high-wing parasol monoplane of mixed construction.

The series was built from 1931 to 1932, numbered from 5-1 to 5-80.

A variant of PWS-10 was a biplane PWS-15, being PWS-10 with another pair of wings.

A single prototype was made to compare with a monoplane, on the factory’s initiative.

It first flew in the spring of 1931.

It offered better manoeuvrability and climb ratio with a slightly lower maximum speed.

PWS-15 was not produced and was soon broken up.

Variants

PWS-10

Single-seat fighter biplane.

PWS-10M

This was the original designation of the PWS-10.

PWS-15

PWS-10 with a new wing, one conversion only, not successful.

Specifications

Crew

1

Length

7.7 m (25 ft 3 in)

Wingspan

10.5 m (34 ft 5 in)

Height

2.9 m (9 ft 6 in)

Wing area

18.25 m2 (196.4 sq ft)

Empty weight

1,113 kg (2,454 lb)

Gross weight

1,500 kg (3,307 lb)

Max take-off weight

1,550 kg (3,417 lb)

Powerplant

1 × Lorraine-Dietrich 12Eb,

W-12 water-cooled piston engine,

356 kW (478 hp)

Propellers

2-bladed fixed-pitch propeller

Performance

Maximum speed

240 km/h (150 mph, 130 kn)

Cruise speed

215 km/h (134 mph, 116 kn)

Range

520 km (320 mi, 280 nmi)

Service ceiling

5,900 m (19,400 ft)

Rate of climb

5.8 m/s (1,140 ft/min)

Wing loading

82.3 kg/m2 (16.9 lb/sq ft)

Armament

Guns

2 x 7.7 mm Vickers machine guns.

 

 

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