Aero Ae 04

The Aero Ae 04 was a Czechoslovakian biplane fighter aircraft of 1921. A development of the Ae 02, it was no more successful than its predecessor in attracting purchase orders, and it flew only in prototype form. Undaunted by the lack of interest, development continued as the A.18.

pecifications (Ae 04)

aircraft specifications
plane or copter?=plane
jet or prop?=prop
ref=
crew=one, pilot
capacity=
payload main=
payload alt=
length main= 5.60 m
length alt= 18 ft 4 in
span main= 7.70 m
span alt= 25 ft 3 in
height main= 2.70 m
height alt= 8 ft 10 in
area main= 14.6 m²
area alt= 157 ft²
airfoil=
empty weight main= 670 kg
empty weight alt= 1,474 lb
loaded weight main=
loaded weight alt=
useful load main=
useful load alt=
max takeoff weight main= 900 kg
max takeoff weight alt= 1,980 lb
more general=
engine (prop)= BMW IIIa
type of prop=
number of props=1
power main= 138 kW
power alt= 185 hp
power original=
max speed main=225 km/h
max speed alt= 69 mph
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= 6,362 m
ceiling alt= 20,876 ft
climb rate main= 357 m/min
climb rate alt= 1,171 ft/min
loading main=
loading alt=
thrust/weight=
power/mass main=
power/mass alt=
more performance=
armament=
* 2 x synchronised .303 Vickers machine guns
avionics=

ee also

aircontent
related=
Aero Ae 02 -
Aero A.18

similar aircraft=

lists=

see also=