AEG B.I

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

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caption =
designer =
first flight =1914
introduced =1914
retired =
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produced =
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The AEG B.I was a German two-seat biplane unarmed reconnaissance aircraft produced in very small numbers from 1914. It formed the basis for the more successful B- and C-type aircraft from AEG.

Operators

*flag|German Empire: Luftstreitkräfte

pecifications (B.I)

Aircraft specification

plane or copter?=plane
jet or prop?=prop
ref=
crew=Two
length main=10.5 m
length alt=34 ft 5 in
span main=14.5 m
span alt=47 ft 7 in
height main=
height alt=
area main=44 m²
area alt=473 ft²
empty weight main=744 kg
empty weight alt=1,640 lb
loaded weight main=
loaded weight alt=
max takeoff weight main=1,040 kg
max takeoff weight alt=2,290 lb
engine (prop)=Mercedes D.I
type of prop=inline engine
number of props=1
power main=74.5 kW
power alt=100 hp
max speed main=100 km/h
max speed alt=62 mph
range main=
range alt=
ceiling main=2,500 m
ceiling alt=8,202 ft
climb rate main=
climb rate alt=
loading main=24 kg/m²
loading alt=4.92 lb/ft²
power/mass main=
power/mass alt=

External links

* [http://www.luftfahrtmuseum.com/htmi/itf/aegb1.htm AEG B.I at the Virtual Aviation Museum]

ee also

aircontent
related=
similar aircraft=
sequence=AEG B.I -
AEG B.II -
AEG B.III