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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
VariantAGO C.II

TheAGO C.I was aFirst World War Germanpusher reconnaissancebiplane that used a pod-and-boom configuration.

Development

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The crew andpusher 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 amachine gun.[1]

A single example was fitted with floats for coastal patrol duties for theImperial German Navy (designationC.I-W).

Operators

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German Empire

Specifications

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AGO C.I

Data from Ago C.I[2]

General characteristics

  • Crew: two, pilot and observer
  • Length: 9.30 m (30 ft 6 in)
  • Wingspan: 15.10 m (49 ft 6 in)
  • Height: 3.10 m (10 ft 2 in)
  • Wing area: 47.6 m2 (512 sq ft)
  • Empty weight: 960 kg (2,116 lb)
  • Gross weight: 1,495 kg (3,296 lb)
  • Powerplant: 1 ×Mercedes D.III , 120 kW (160 hp)

Performance

  • Maximum speed: 130 km/h (81 mph, 70 kn)
  • Range: 480 km (300 mi, 260 nmi)
  • Endurance: 3 hr[3]
  • Time to altitude: 9.5 min to 1,000 m (3,300 ft)

Armament

See also

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Aircraft of comparable role, configuration, and era

References

[edit]
Wikimedia Commons has media related toAGO C.I.

Citations

[edit]
  1. ^van Wyngarden, G (2006). Early German Aces of World War I, Osprey Publishing Ltd.ISBN 1-84176-997-5
  2. ^Grosz 1999, p. 32.
  3. ^Hornát 2001, p. 530.

Bibliography

[edit]
  • Grosz, Peter M. (1999).Ago C.I. Windsock Datafile No. 75. Albatros Productions.ISBN 978-1902207162.
  • Hornát, Jiří (2001). "Letadla 14–18: AGO C.I".Letectví + Kosmonautika (in Czech). Vol. LXXVII, no. 8. p. 530.ISSN 0024-1156.
  • Taylor, Michael J. H. (1989).Jane's Encyclopedia of Aviation. London: Studio Editions. p. 39.
  • "Das Virtuelle Luftfahrtmuseum".
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