Fieseler Fi 157

Fieseler Fi 157

Infobox Aircraft
name=Fieseler Fi 157


caption=
type=Unmanned anti-aircraft target drone
manufacturer=Fieseler
designer=
first flight=1937
introduced=
retired=
status=
primary user=
more users=
produced=
number built=
program cost=
unit cost=
developed from=
variants with their own articles=
The Fieseler Fi 157 was an unsuccessful attempt at developing a radio-controlled, full-sized anti-aircraft target.

Development

In 1937, the Reichsluftfahrtministerium (RLM) contracted Fieseler to produce a radio controlled anti-aircraft target drone. The resulting Fi 157 was a low-wing monoplane of entirely wooden construction and was carried beneath a bomber before being released. All three prototypes crashed during testing; a single example of a manned version, designated the Fi 158, was built to investigate remote guidance.

pecifications (Fieseler Fi 157)

aircraft specifications

plane or copter?=plane
jet or prop?=prop

ref=

crew=
capacity=
length main=6.6 m
length alt=22 ft
span main=7.0 m
span alt=23 ft
height main=1.7 m
height alt=6 ft
area main= m²
area alt= ft²
airfoil=
empty weight main=494 kg
empty weight alt=1,090 lb
loaded weight main=646 kg
loaded weight alt=1,420 lb
useful load main=
useful load alt=
max takeoff weight main=
max takeoff weight alt=
more general=

engine (prop)=Hirth HM 506A
type of prop=
number of props=
power main=160 hp
power alt=120 kW

max speed main=350 km/h
max speed alt=190 knots, 220 mph
cruise speed main=300 km/h
cruise speed alt=160 knots, 190 mph
stall speed main=
stall speed alt=
never exceed speed main=
never exceed speed alt=
range main=370 km
range alt=200 nm, 230 mi
ceiling main= m
ceiling alt= ft
climb rate main=
climb rate alt=
loading main=
loading alt=
power/mass main=
power/mass alt=
more performance=

armament=

avionics=

References

# "Facts by request: reply to "A 'sporting' target". "Flying Review International". July 1969, p. 65.


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