AEG G.II

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The AEG G.II was a biplane bomber aircraft of World War I developed from the AEG G.I. With more powerful engines, the twenty-four aircraft built featured performance adequate enough to enable them to see some limited operational use.

Contents

[edit] Specifications (AEG G.II)

[edit] General characteristics

  • Crew: three
  • Length: 9.10 m (29 ft 10 in)
  • Wingspan: 16.20 m (53 ft 2 in)
  • Height: 3.49 m (11 ft 5 in)
  • Wing area: 59 m² (635 ft²)
  • Empty: 1,450 kg (3,197 lb)
  • Loaded: kg ( lb)
  • Maximum takeoff: 2,470 kg (5,446 lb)
  • Powerplant: 2x Benz Bz III, 112 kW (150 hp) each

[edit] Performance

  • Maximum speed: 140 km/h (88 mph)
  • Range: 700 km (438 miles)
  • Service ceiling: 3,000 m (9,843 ft)
  • Rate of climb: 90 m/min (295 ft/min)
  • Wing loading: kg/m² ( lb/ft²)
  • Power/Mass: kW/kg ( hp/lb)

[edit] Armament

[edit] Related content

Related development:

Comparable aircraft:
Friedrichshafen G series: Friedrichshafen G.I, G.II, G.III, G.IV,
Gotha G series: Gotha G.I, G.II, G.III, G.IV, G.V|

Designation sequence: AEG G.I - AEG G.II - AEG G.III - AEG G.IV - AEG G.V