AEG C.V
The AEG C.V was a prototype two-seat biplane reconnaissance aircraft of World War I. A single AEG C.IV was modified to utilise a more powerful engine, but the results were disappointing enough that further development was cancelled.
Specifications (AEG C.V)General Characteristics Crew: two, pilot and observer Length: 7.16 m (23 ft 6 in) Wingspan: 13.46 m (44 ft 2 in) Height: 3.35 m (11 ft) Wing area: 39 m² (420 ft²) Empty: 802 kg (1,764 lb) Loaded: kg ( kg) Maximum takeoff: 1,120 kg (2,464 lb) Powerplant: 1x Mercedes D.IV, 164 kW (220 hp)
Performance Maximum speed: km/h ( mph) Range: km ( miles) Service ceiling: m ( ft) Rate of climb: m/min ( ft/min) Wing loading: kg/m² ( lb/ft²) Power/Mass: kW/kg ( hp/lb)
Armament 1x forward-firing 7.92mm LMG 08/15 machine gun 1x 7.92 mm Parabellum machine gun in ring mount for observer
Related content
Related development:
AEG C.IV Comparable aircraft: Designation sequence:
AEG C.II -
AEG C.III -
AEG C.IV -
AEG C.V -
AEG C.VI -
AEG C.VII -
AEG C.VIII -
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