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AEG C.VIII

During World War I, the AEG C.VIII emerged as a prototype aircraft specifically designed for reconnaissance purposes.

This aircraft, which was built in two variations, drew inspiration from the well-received C.IV design.

The first variant featured a biplane configuration, while the second variant boasted a triplane design.

Despite the efforts put into the development of the AEG C.VIII, neither version managed to significantly surpass the capabilities of its predecessor, the C.IV.

As a result, the potential for mass production of these aircraft was deemed unworthy.

The limited advancements offered by the C.VIII failed to justify the resources and investments required for large-scale manufacturing.

The AEG C.VIII, a notable prototype aircraft from World War I, aimed to serve as a reconnaissance plane.

It was constructed in two distinct versions, both of which were based on the successful C.IV design.

However, neither the biplane nor the triplane variant showcased substantial improvements over the C.IV model, rendering the idea of mass production unfeasible.

The lack of significant advancements in the C.VIII’s performance and capabilities ultimately led to its limited production and deployment during the war.

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

Specifications

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 inline 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

4.386 m/s (863.4 ft/min)

Power/mass

0.10 kW/kg (0.061 hp/lb).

 

 

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