The Udet U 11 Kondor was a German four-engined airliner designed and built by Udet Flugzeugbau, only one was built.[1][2]

U 11 Kondor
Role	Eight-seat airliner Type of aircraft
National origin	Germany
Manufacturer	Udet Flugzeugbau
First flight	19 January 1926
Primary user	Deutsche Luft Hansa
Number built	1

Design and development

The U 11 Kondor was an open-cockpit, metal-fuselage, wooden high-wing monoplane powered by four 100 hp (75 kW) Siemens-Halske Sh 12 piston engines in shaft-driven pusher configuration.[1] It had a crew of three and room for eight passengers with a dangerously close clearance between the pusher propellers and rear passenger door, which caused one fatality.[1] The aircraft was tested by Harry Rother near Munich, finding a tail-heavy condition which required addition of larger control surfaces. The only U 11 was first flown on 19 January 1926 and was refused by Deutsche Luft-Reederei then purchased by Deutsche Luft Hansa, crashing on its delivery flight. The cost to develop and produce the prototype was a factor in the collapse of the company, which was then taken over by Bayerische Flugzeugwerke.[1]

Specifications (U 11)

General characteristics

• Crew: 2
• Capacity: 8
• Length: 16 m (52 ft 6 in)
• Upper wingspan: 22 m (72 ft 2 in)
• Height: 4 m (13 ft 1 in)
• Wing area: 70 m² (750 sq ft)
• Empty weight: 3,370 kg (7,430 lb)
• Gross weight: 4,572 kg (10,080 lb)
• Fuel capacity: 300 kg
• Powerplant: 4 × Siemens-Halske Sh 12 9-cyl. air-cooled radial piston engines, 75 kW (100 hp) each

Performance

• Maximum speed: 152 km/h (94 mph, 82 kn)
• Cruise speed: 135 km/h (84 mph, 73 kn)
• Service ceiling: 3,190 m (10,470 ft)

See also

Aircraft of comparable role, configuration, and era

• Stout 3-AT A similar all-metal three-engine design developed in America
• Fokker F.VII German airliner

References

Notes

Bibliography

External links

Wikimedia Commons has media related to Udet U 11 Kondor.

• Udet U 11
• Flickr Photo

На других языках

[de] Udet U 11