AEG C.V
From Wikipedia, the free encyclopedia
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.
[edit] 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 weight: 802 kg (1,764 lb)
- Max takeoff weight: 1,120 kg (2,464 lb)
- Powerplant: 1× Mercedes D.IV 8-cylinder, liquid-cooled, inline engine, 164 kW (220 hp)
Performance
Armament
- 1 × forward-firing 7.92mm LMG 08/15 machine gun
- 1 × 7.92 mm Parabellum MG14 machine gun in ring mount for observer
[edit] See also
Related development AEG C.IV
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