AEG C.II

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The AEG C.II was a two-seat biplane reconnaissance aircraft produced in small numbers from October 1915. It was a slightly smaller version of the C.I with slightly better performance.

Contents

Specifications (AEG C.II)

General characteristics

  • Crew: two, pilot and observer
  • Length: 7.09 m (23 ft 3 in)
  • Wingspan: 11.95 m (39 ft 2 in)
  • Height: m ( ft in)
  • Wing area: m² ( ft²)
  • Empty: 680 kg (1,450 lb)
  • Loaded: kg ( lb)
  • Maximum takeoff: 1,200 kg (2,646 lb)
  • Powerplant: 1x Benz Bz.III, 112 kW (150 hp)

Performance

  • Maximum speed: 140 km/h (87 mph)
  • Range: km ( miles)
  • Service ceiling: m ( ft)
  • Rate of climb: m/min ( ft/min)
  • Wing loading: kg/m² ( lb/ft²)
  • Power/mass: W/kg ( hp/lb)

Armament

See also

Related development:

Comparable aircraft:

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


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