| C.VIII | |
|---|---|
![]()  | |
| Role | Reconnaissance aircraft | 
| National origin | |
| Manufacturer | AEG | 
| First flight | October 1917 | 
| Primary user | Luftstreitkräfte | 
| Number built | 2 | 
| Developed from | AEG C.IV | 
The AEG C.VIII was a prototype two-seat reconnaissance aircraft of World War I.[1] Two examples were built, based on the successful C.IV design, one of biplane configuration, the other a triplane (the latter sometimes referred to as the C.VIII.Dr). Neither version offered enough of an improvement on the C.IV to make mass production worthwhile.
Variants
- C.VIII - Biplane prototype two-seater fighter/reconnaissance aircraft.
 - C.VIII Dr - Triplane version of C.VIII, no improvement in climb and speed reduced to 165 km/h (103.12 mph)
 
Specifications (AEG C.VIII)
Data from German Aircraft of the First World War [1]
General characteristics
- Crew: 2
 - Length: 6.9 m (22 ft 8 in)
 - Wingspan: 9.5 m (31 ft 2 in)
 - Empty weight: 800 kg (1,764 lb)
 - Gross weight: 1,160 kg (2,557 lb)
 - Powerplant: 1 × Mercedes D.III 6-cylinder water-cooled in-line piston engine, 120 kW (160 hp)
 - Propellers: 2-bladed fixed-pitch propeller
 
Performance
- Maximum speed: 170 km/h (110 mph, 92 kn)
 - Rate of climb: 4.4 m/s (870 ft/min)
 - Power/mass: 0.10 kW/kg (0.061 hp/lb)
 
See also
Related development
Aircraft of comparable role, configuration, and era
Related lists
References
Wikimedia Commons has media related to AEG C.VIII.
- Gray, Peter and Thetford, Owen. German Aircraft of the First World War. London:Putnam, 1970 2nd. Ed.
 
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