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AEG C.VII

From Wikipedia, the free encyclopedia
Reconnaissance biplane prototype model by AEG
C.VII
The third prototype C.VII with the swept wing
General information
TypeReconnaissance aircraft
National originGerman Empire
ManufacturerAllgemeine Elektricitäts-Gesellschaft
Number built3
History
First flightDecember 1916
Developed fromAEG C.IV
One of the first two prototype C.VIIs with the straight upper wing

TheAEG C.VII was aprototype two-seatbiplanereconnaissance aircraft built by theAllgemeine Elektricitäts-Gesellschaft (AEG) during theFirst World War for theImperial German Army's (Deutsches Heer)Imperial German Air Service (Luftstreitkräfte). It was developed from theC.IV but did not enter production. The C.VII was tested with two different wing arrangements, one with straight wings and another with a swept upper wing.

Development

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The C.VII had been developed to the Inspectorate of Flying Troops (Inspektion der Fliegertruppen (Idflieg)'s requirement for a new type of two-seat aircraft, smaller than the existing C-type aircraft. These were to be used to equip protection flights (Schutzstaffeln) to escort reconnaissance aircraft.[1] Three prototypes were ordered in October 1916 with the first aircraft completed in December. They were scaled down about 20 percent from the C.IV and the C.VII hadsingle-bay wings. The two aircraft shared the same water-cooled 160-horsepower (120 kW)Mercedes D.IIIstraight-six piston engine and the armament of one fixed, forward-firing machine gun and another on a flexible mount for theobserver. The C.VII was about 20 kilometers per hour (12 mph) faster than the C.IV and had a better rate of climb. The first two prototypes had upper wings with straightleading edges, but the third had a swept wing that was intended to improve the gunner's visibility.[2]

Fight testing was conducted in early 1917;Idflieg's report of 30 April damned the C.VII with faint praise, saying that its performance was acceptable, but was not as good as expected. It was judged suitable for service on the less demandingEastern Front and inferior to the submissions byHannoversche Waggonfabrik andHalberstädter Flugzeugwerke.[3]

Specifications (AEG C.VII)

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Data from German Aircraft of the First World War;[4] A.E.G. Aircraft of WWI: A Centennial Perspective on Great War Airplanes[5]

General characteristics

  • Crew: 2
  • Length: 6.2 m (20 ft 4 in)
  • Upper wingspan: 11.1 m (36 ft 5 in)
  • Lower wingspan: 10.05 m (33 ft 0 in)
  • Wing area: 26 m2 (280 sq ft)
  • Empty weight: 758 kg (1,671 lb)
  • Gross weight: 1,118 kg (2,465 lb)
  • Powerplant: 1 ×Mercedes D.III water-cooledstraight-six piston engine, 120 kW (160 hp)
  • Propellers: 2-bladed

Performance

  • Maximum speed: 175 km/h (109 mph, 94 kn)
  • Time to altitude: 4 minutes to 1,000 m (3,300 ft)

Armament

  • Guns: * 1 × forward-firing 7.92 mm (.312 in)LMG 08/15 machine gun
  • 1 × 7.92 mm (.312 in)Parabellum MG 14 machine gun in ring mount for observer

See also

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Related development

Related lists

References

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  1. ^Gray & Thetford, p. xv
  2. ^Herris, pp. 16–17, 44
  3. ^Herris, p. 44
  4. ^Gray & Thetford, p. 236
  5. ^Herris, p. 17

Bibliography

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Wikimedia Commons has media related toAEG C.VII.
  • Gray, Peter & Thetford, Owen (1987) [1970].German Aircraft of the First World War (2nd ed.). London: Putnam.ISBN 0-85177-809-7.
  • Herris, Jack (2015).A.E.G. Aircraft of WWI: A Centennial Perspective on Great War Airplanes. Great War Aviation Centennial Series. Vol. 16. n. p.: Aeronaut Books.ISBN 978-1-935881-28-5.
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