PZL.38 Wilk
PZL.38 Wilk | |
---|---|
PZL.38 | |
Role | Heavy fighter |
Manufacturer | Państwowe Zakłady Lotnicze |
First flight | 1938 |
Number built | 2 |
Variants | PZL.48 Lampart |
The PZL.38 Wilk (wolf) (PZL-38) was a Polish heavy fighter developed and manufactured by PZL state factory in 1937. Intended for use primarily as a fighter-bomber, the Polish Air Force also envisioned it replacing light fighters in long-range operations, along with being able to serve as a light bomber. Only two examples were built before the project was cancelled in favor of a planned improved variant, the PZL.48 Lampart (itself never built owing to the outbreak of WWII).
Design and development
In 1934 the
In 1937 two prototypes of PZL.38 were built. The second one (PZl.38/II) received the American Ranger SGV-770B engines (420-450 hp), which were less powerful than the PZL "Foka" engine. As a result, the prototype didn't meet expected performance. The second prototype flew first in April or May 1936. The first prototype PZl.38/I, received the PZL Foka engine. The airplane was shown in 1938 at the Paris Air Show. It was flown only in February or March 1939 and also did not meet expected performance (estimated maximum speed was 520 km/h, while it hardly reached 465 km/h). It was also too heavy (2155 kg instead of 1715 kg) and had too small useful load. Because of these facts, further development of PZL.38 "Wilk" aircraft and "Foka" engine was abandoned in the spring of 1939, in a favour of the new construction PZL.48 "Lampart" - which was a modification of "Wilk" with radial engines.
Description
It was a twin-engine low-wing cantilever
Operational history
At the time of the German
Specifications
Data from Polish Aircraft 1893–1939[1]
General characteristics
- Crew: 2, pilot, rear gunner/bombardier
- Length: 8.35 m (27 ft 5 in)
- Wingspan: 11.05 m (36 ft 3 in)
- Height: 2.50 m (8 ft 2 in)
- Wing area: 19.0 m2 (205 sq ft)
- Aspect ratio: 6.43
- Empty weight: 1,715 kg (3,781 lb)
- Gross weight: 2,770 kg (6,107 lb)
- Powerplant: 2 × V-engine, 310 kW (420 hp) each
- Propellers: 2-bladed
Performance
- Maximum speed: 465 km/h (289 mph, 251 kn) at 4,000 m (13,000 ft)
- Cruise speed: 400 km/h (250 mph, 220 kn) at sea level
- Range: 1,250 km (780 mi, 670 nmi)
- Service ceiling: 10,000 m (33,000 ft) estimated
- Wing loading: 146 kg/m2 (30 lb/sq ft)
- Power/mass: 0.22 kw/kg (0.13 hp/lb)
Armament
- 1 x 20 mm FK-A cannon fixed in nose
- 2 x 7.92 mm PWU wz.36machine guns fixed in nose
- 2 x 7.92 mm PWU wz.37machine guns movable at the upper rear
- 300 kg bombs
See also
Related development
- PZL.48 Lampart
- PZL.54 Ryś
Aircraft of comparable role, configuration, and era
References
- ^ Cynk 1971, pp. 240–241, 243
- Cynk, Jerzy B. Polish Aircraft 1893–1939. London: Putnam, 1971. ISBN 0-370-00085-4.
- Glass, Andrzej. Polskie Konstrukcje Lotnicze 1893-1939 (Polish aviation constructions 1893-1939). Warsawa, Poland: WKiŁ, 1977. (Polish language, no ISBN)
- Glass, Andrzej. PZL 38 Wilk. Warsawa, Poland: Wydawnictwo Militaria, 1995. ISBN 83-86209-41-0. (Polish language)
External links
- PZL.38 translated description, photos and drawings at Ugolok Neba