AEG B.II

infobox Aircraft
name =B.II
type =Reconnaissance aircraft
manufacturer =AEG


caption =
designer =
first flight =1914
introduced =1914
retired =
status =
primary user =
more users =
produced =
number built =
unit cost =
variants with their own articles =

The AEG B.II was a two-seat biplane reconnaissance aircraft produced in small numbers from 1914. It was a slightly smaller version of the B.I and proved more successful. They were used in limited numbers throughout 1914/1915, but wound up quickly replaced, as they were often derided for lack of speed and armament.

Operators

*flag|German Empire: Luftstreitkräfte

pecifications (B.II)

Aircraft specification

plane or copter?=plane
jet or prop?=prop
ref=
crew=Two
length main=10.5 m
length alt=34 ft 5.5 in
span main=15.5 m
span alt=50 ft 10 in
height main=3.15 m
height alt=10 ft 4 in
area main=40.12 m²
area alt=431.8 ft²
empty weight main=723 kg
empty weight alt=1,594 lb
loaded weight main=
loaded weight alt=
useful load main=348 kg
useful load alt=767 lb
max takeoff weight main=650 kg
max takeoff weight alt=1,433 lb
engine (prop)=Mercedes D.II
type of prop=inline engine
number of props=1
power main=89.5 kW
power alt=120 hp
max speed main=110 km/h
max speed alt=68 mph
cruise speed main=110 km/h
cruise speed alt=68 mph
range main=1,130 km
range alt=700 miles
ceiling main=3,000 m
ceiling alt=9,800 ft
climb rate main=
climb rate alt=
loading main=27 kg/m²
loading alt=5.54 lb/ft²
power/mass main=
power/mass alt=

External links

* [http://www.luftfahrtmuseum.com/htmi/itf/aegb2.htm AEG B.II at the Virtual Aviation Museum]

ee also

aircontent
related=
AEG C.I

similar aircraft=