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AEG J.I
From Wikipedia, the free encyclopedia
This aircraft article is missing some (or all) of its specifications. If you have a source, you can help Wikipedia by adding them.The AEG J.I was a biplane ground attack aircraft of 1916, a development of the AEG C.IV reconnaissance aircraft. It featured armour protection for the pilot and for the more powerful engine that was fitted to the heavier aircraft.
Contents |
- Crew: two
- Length: 7.20 m (23 ft 7 in)
- Wingspan: 13.46 m (44 ft 2 in)
- Height: 3.35 m (11 ft)
- Wing area: 33.2 m² (357 ft²)
- Empty: 1,455 kg (3,201 lb)
- Loaded: kg ( lb)
- Maximum takeoff: 1,740 kg (3,828 lb)
- Powerplant: 1x Benz Bz.IV, 149 kW (200 hp)
- Maximum speed: 150 km/h (94 mph)
- Range: 375 km (234 miles)
- Service ceiling: 4,500 m (14,760 ft)
- Rate of climb: 168 m/min (551 ft/min)
- Wing loading: kg/m² ( lb/ft²)
- Power/Mass: kW/kg ( hp/lb)
- 2x 7.92 mm LMG 08/15 machine guns
- 1x 7.92 mm Parabellum machine gun
Related development: AEG C.IV
Comparable aircraft:
Designation sequence: AEG J.I - AEG J.II
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