AEG C.V
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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.
Contents
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.IVComparable 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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