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.
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Specifications (AEG G.II)
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
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)
Armament
- 2x 7.92mm machine guns
- 200 kg (440 lb) of bombs
Related content
Related development:Comparable aircraft:
Designation sequence: AEG G.I - AEG G.II - AEG G.III - AEG G.IV - AEG G.V
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