AEG C.VIII
The AEG C.VIII was a prototype two-seat reconnaissance aircraft built by the Script error: No such module "Lang". (AEG) during the First World War for the Imperial German Army's (Script error: No such module "Lang".) Imperial German Air Service (Script error: No such module "Lang".). Three examples were built in an effort to improve on the unsuccessful C.VII design, two of biplane configuration, the other a triplane (the latter sometimes referred to as the C.VIII.Dr). Neither version offered enough of an improvement over aircraft already in service to make mass production worthwhile.
Development
The C.VII had been developed to the Inspectorate of Flying Troops (Script error: No such module "Lang". (Script error: No such module "Lang".)'s requirement for a new type of two-seat aircraft, smaller than the existing C-type aircraft. These were to be used to equip protection flights (Script error: No such module "Lang".) to escort reconnaissance aircraft.[1] The C.VII had proven inferior to the submissions by Script error: No such module "Lang". and Script error: No such module "Lang"., but AEG hoped that a more aerodynamic version of the C.VII might be successful. Script error: No such module "Lang". ordered three prototypes in mid-1917 and AEG decided to build one as a triplane to appeal to Script error: No such module "Lang".'s fascination with triplanes at that time.[2]
Changes to the C.VIII included new multi-wing spars, tall "ear"-type radiators mounted on the sides of the fuselage, a new tail structure with the horizontal stabilizers supported by two struts and a single interplane I-strut supporting the wings. The first of the biplanes was completed in July 1917. The triplane used the fuselage, engine and tail of the biplanes. An extra I-strut was added to support the extra weight of the wings. Neither design proved superior to the designs from other companies and they did not enter production.[3][2]
Variants
- C.VIII - Biplane prototype two-seater fighter/reconnaissance aircraft.[3]
- C.VIII Dr - Triplane version of C.VIII, no improvement in climb and speed reduced to 165 km/h (103.12 mph)[3]
Specifications (C.VIII)
See also
Aircraft of comparable role, configuration, and era
Related lists
References
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Bibliography
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