Junkers Ju 187
infobox Aircraft
name =Ju 187
type =
manufacturer =Junkers
caption =
designer =
first flight =
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retired =
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more users =
produced =
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variants with their own articles =
The Junkers Ju 187 was designed to replace the aging
The project was cancelled by the
pecifications (Ju 187)
aircraft specifications
plane or copter?=plane
jet or prop?=prop
ref=
crew=2 (pilot and gunner)
capacity=
payload main=
payload alt=
length main=11.80 m
length alt=38 ft 8¾ in
span main=18.06 m
span alt=59 ft 3¼ in
height main=3.90 m
height alt=12 ft 9¾ in
area main=
area alt=
airfoil=
empty weight main=
empty weight alt=
loaded weight main=
loaded weight alt=
useful load main=
useful load alt=
max takeoff weight main=
max takeoff weight alt=
more general=
engine (prop)=
type of prop=12-cylinder inverted-vee engine
number of props=1
power main=1,324 kW
power alt=1,776 hp
power original=
max speed main=400 km/h
max speed alt=249 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=
ceiling alt=
climb rate main=
climb rate alt=
loading main=
loading alt=
thrust/weight=
power/mass main=
power/mass alt=
more performance=
armament=
* 2 x 20 mm MG 151/20 cannon in wing roots
* 1 x 13 mm
* 1 x 20 mm MG 151/20 cannon in dorsal turret
* 1 x 1,000 kg (2,204 lb) bomb in semi recessed bay
* 4 x 50 kg (120 lb) bombs on external wing racks
avionics=
ee also
Related development:
*
References
D. Herwig & H. Rode "Luftwaffe Secret Projects - Ground Attack & Special Purpose Aircraft". ISBN 1-85780-150-4
External links
* [http://www.luft46.com/junkers/ju187.html Luft 46 Entry]