Jump to content

AGO C.I

From Wikipedia, the free encyclopedia
C.I
Forward oblique view of the AGO C.I
General information
TypeReconnaissance
ManufacturerAGO Flugzeugwerke
Designer
August Häfeli
Primary userGermany
Number built64
History
Introduction dateJune 1915
VariantsAGO C.II

The AGO C.I was a First World War German pusher reconnaissance biplane that used a pod-and-boom configuration.

Development

[edit]

The crew and pusher engine shared a central nacelle, and the twin booms carried the tail and the four-wheeled landing gear. The observer sat at the nose and was armed with a machine-gun.[1]

A single example was fitted with floats for coastal patrol duties for the Imperial German Navy (designation C.I-W).

Operators

[edit]
 German Empire

Specifications

[edit]
AGO C.I

General characteristics

  • Crew: two, pilot and observer
  • Length: 9.0 m (29 ft 6 in)
  • Wingspan: 15.0 m (49 ft 2 in)
  • Wing area: 41.5 m2 (447 sq ft)
  • Powerplant: 1 × Mercedes D.III , 117 kW (158 hp)

Performance

  • Maximum speed: 140 km/h (90 mph, 78 kn)
  • Range: 480 km (300 mi, 260 nmi)
  • Service ceiling: 4,800 m (16,000 ft)

Armament

See also

[edit]

Aircraft of comparable role, configuration, and era

References

[edit]

Citations

[edit]
  1. ^ van Wyngarden, G (2006). Early German Aces of World War I, Osprey Publishing Ltd. ISBN 1-84176-997-5

Bibliography

[edit]