LWS-6 Żubr

· LWS · 2 × Bristol Pegasus

Airplanes

Length

15.4 m

Flat Wing Span

18.5 m

Height

3.5 m

Flat Wing Area

49.5 m²

Cruise Speed

300 km/h

Max Speed

380 km/h

Max Ceiling

8000 m

Number of Engines

Aircraft Engine

First Flight

1936-03-01

Entry Into service

1938-01-01

Number Built

Maximum Take-Off Weight

6.876 t (paragliders: kg)

Maximum Range

1250 km

Pictures

No pictures yet for this family.

Aircraft	Maximum Take-Off Weight (t (paragliders: kg))	Maximum Range (km)
LWS-6 Żubr	6.876	1250

Name	Aircraft Engine	Length (m)	Flat Wing Span (m)	Max Seating
Aircraft Industries L 410 NG		15.074	19.478	19	Compare
Henschel Hs 124		14.5	18.2		Compare
FMA IA 50 Guaraní II	Turbomeca Bastan	14.86	19.53	15	Compare
Tupolev ANT-35		15.4	20.8		Compare
Indonesian Aerospace N219		16.49	19.5	19	Compare
Heinkel He 219 Uhu		15.33	18.5		Compare

All data (23 fields)

Name: LWS-6 Żubr
Manufacturer: LWS
Description: The LWS-6 Żubr (PZL.30, wisent) was a twin-engined medium bomber designed and produced by the Polish aircraft manufacturer LWS.
First Flight: 1936-03-01
Entry Into service: 1938-01-01
Designer: LWS
Type: Medium bomber
Length (m): 15.4
Height (m): 3.5
Cockpit Crew: 4
Max Speed (km/h): 380
Cruise Speed (km/h): 300
Max Ceiling (m): 8000
Rate of Climb (m/s): 6.8
Armament: 2 × 7.7 mm Vickers F machine guns in nose turret; 2 × 7.7 mm Vickers F machine guns in upper dorsal rear turret; 1 × 7.7 mm Vickers F machine gun in ventral underbelly position; 660 kg (1,450 lb) of bombs
Number Built: 17
Powerplant Description: 2 × PZL Pegasus VIII nine-cylinder air-cooled radial piston engines, 492 kW (660 hp) each
Primary Users: Polish Air Force, Luftwaffe , Soviet Air Forces
Wikipedia Article (URL): en.wikipedia.org/wiki/LWS-6_%C5%BBubr
Flat Wing Span (m): 18.5
Flat Wing Area (m²): 49.5
Aircraft Engine: Bristol Pegasus
Number of Engines: 2