AEG C.V

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.

pecifications (AEG C.V)

aircraft specifications
plane or copter?= plane
jet or prop?= prop
ref=
crew=two, pilot and observer
capacity=
length main= 7.16 m
length alt= 23 ft 6 in
span main= 13.46 m
span alt= 44 ft 2 in
height main= 3.35 m
height alt= 11 ft
area main= 39 m²
area alt= 420 ft²
airfoil=
empty weight main= 802 kg
empty weight alt= 1,764 lb
loaded weight main=
loaded weight alt=
useful load main=
useful load alt=
max takeoff weight main= 1,120 kg
max takeoff weight alt= 2,464 lb
more general=
engine (prop)=Mercedes D.IV
type of prop=8-cylinder, liquid-cooled, inline engine
number of props=1
power main= 164 kW
power alt= 220 hp
power original=
max speed main=
max speed alt=
cruise speed main=
cruise speed alt=
stall speed main=
stall speed alt=
never exceed speed main=
never exceed speed alt=
range main=
range alt=
ceiling main=
ceiling alt=
climb rate main=
climb rate alt=
loading main=
loading alt=
thrust/weight=
power/mass main=
power/mass alt=
more performance=
armament=
* 1 × forward-firing 7.92 mm LMG 08/15 machine gun
* 1 × 7.92 mm Parabellum MG14 machine gun in ring mount for observer
avionics=

ee also

aircontent
related=
AEG C.IV
similar aircraft=
lists=
* List of military aircraft of Germany
see also=