Udet U 11 Kondor

Last updated
U 11 Kondor
Udet U 11 Kondor Aero Digest June 1926.jpg
General information
TypeEight-seat airliner
National origin Germany
Manufacturer Udet Flugzeugbau
Primary user Deutsche Luft Hansa
Number built1
History
First flight19 January 1926

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

Contents

Design and development

The U 11 Kondor [3] [4] 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)

Udet U 11 Kondor 3-view drawing from Les Ailes February 11, 1926 Udet U 11 Kondor 3-view Les Ailes February 11,1926.png
Udet U 11 Kondor 3-view drawing from Les Ailes February 11, 1926

General characteristics

Performance

See also

Aircraft of comparable role, configuration, and era

References

Notes

  1. 1 2 3 4 Orbis 1985, p. 3035
  2. Jean-Denis G.G. Lepage. Aircraft of the Luftwaffe, 1935-1945: An Illustrated Guide. p. 28.
  3. "U 11 Kondor". Illustrierte Technik für Jedermann. 1926-02-06. Retrieved 2025-08-16.
  4. "Udet U 11 Kondor". Illustrierte Technik für Jedermann. 1926-01-30. Retrieved 2025-08-16.

Bibliography