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C.III | |
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Role | Reconnaissance |
Manufacturer | AGO Flugzeugwerke |
Designer | A. Haefeli |
Primary user | Germany |
The AGO C.III was a German reconnaissance biplane of World War I. It was a single experimental prototype derived from the manufacturer's C.I design.
General characteristics
Performance
Armament
Homo heidelbergensis is an extinct species or subspecies of archaic human which existed during the Middle Pleistocene. It was subsumed as a subspecies of H. erectus in 1950 as H. e. heidelbergensis, but towards the end of the century, it was more widely classified as its own species. It is debated whether or not to constrain H. heidelbergensis to only Europe or to also include African and Asian specimens, and this is further confounded by the type specimen being a jawbone, because jawbones feature few diagnostic traits and are generally missing among Middle Pleistocene specimens. Thus, it is debated if some of these specimens could be split off into their own species or a subspecies of H. erectus. Because the classification is so disputed, the Middle Pleistocene is often called the "muddle in the middle".
The AEG C.II was a German two-seat biplane reconnaissance aircraft produced in small numbers from October 1915. It was a slightly smaller version of the C.I with better performance, redesigned cockpit for both pilot and observer/bombardier, new rear mounting for a 7.92 mm (.312 in) Parabellum MG14 machine gun, and the ability to carry four 10 kg (22 lb) bombs for light attack duties.
The AEG C.III was a two-seat biplane reconnaissance aircraft, a single prototype of which was built during World War I. The aircraft featured an unusual fuselage design that completely filled the gap between the upper and lower sets of wings, to provide the pilot with improved vision, and to allow the observer a wider field of fire for his 7.92 mm (.312 in) machine gun. The pilot sat to the rear of the observer, who was stationed over the upper wing. This design was not as successful as had been hoped, and the C.III was never entered into service. Despite being heavier than the C.II, its maximum speed increased to 158 km/h (98 mph).
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