Hansa-Brandenburg W.13

Hansa-Brandenburg W.13

__NOTOC__ Infobox Aircraft
name=W.13


caption=
type=Flying boat bomber
national origin=Germany
manufacturer=Hansa-Brandenburg, UFAG
designer=Ernst Heinkel
first flight=avyear|1917
introduced=
retired=
status=
primary user=Austro-Hungarian Navy
more users=
produced=
number built=130
variants with their own articles=
The Hansa-Brandenburg W.13 was a flying boat bomber developed in Germany in 1917 and used by the Austro-Hungarian Navy during World War I. It was a largely conventional design for the time, with a single-step hull and an engine mounted pusher-fashion on struts in the interplane gap. The pilot and a gunner sat in tandem open cockpits at the bow. The interplane struts were unusual in that on each side of the aircraft, the upper and lower wings were braced with two pairs of struts that converged from two sets of attachment points on the upper wing to a single set on the lower wing, so that when viewed from fore or aft, the struts formed a V-shape. The type was first offered to the Imperial German Navy, but was rejected. It was, however, accepted by the Austro-Hungarian Navy, which operated it from bases on the Adriatic Sea during the Italian Campaign. Many of these were produced under licence by UFAG in Budapest. In service, the Austro-Daimler engine caused continuous problems, which the manufacturer attributed to the poor lubricating oil available at the front. Since this situation seemed unlikely to change as the war situation deteriorated for Austria-Hungary, Austro-Daimler simply discontinued production of the engine, meaning that slightly over half the 130 W.13s manufactured were left without a powerplant.

Several examples of the W.13 were captured intact by Italian forces and studied; and one example that survived the war was handed over by Austria to the United States Navy as part of war reparations. This aircraft was shipped back to the Naval Aircraft Factory in the United States, where it was dismantled for study, reassembled, and test flown.

pecifications

aerospecs
ref=
met or eng?= met

crew=Two, pilot and gunner
capacity=
length m=13.70
length ft=44
length in=11
span m=20.40
span ft=66
span in=11
swept m=
swept ft=
swept in=
rot number=
rot dia m=
rot dia ft=
rot dia in=
dia m=
dia ft=
dia in=
width m=
width ft=
width in=
height m=4.23
height ft=14
height in=11
wing area sqm=
wing area sqft=
swept area sqm=
swept area sqft=
rot area sqm=
rot area sqft=
volume m3=
volume ft3=
aspect ratio=
empty weight kg=
empty weight lb=
gross weight kg=2,850
gross weight lb=6,280
lift kg=
lift lb=

eng1 number=1
eng1 type=Austro-Daimler 360
eng1 kw= 270
eng1 hp= 360
eng1 kn=
eng1 lbf=
eng1 kn-ab=
eng1 lbf-ab=
eng2 number=
eng2 type=
eng2 kw=
eng2 hp=
eng2 kn=
eng2 lbf=
eng2 kn-ab=
eng2 lbf-ab=

max speed kmh=150
max speed mph=94
max speed mach=
cruise speed kmh=
cruise speed mph=
range km=950
range miles=600
endurance h=
endurance min=
ceiling m=2,000
ceiling ft=610
glide ratio=
climb rate ms=
climb rate ftmin=
sink rate ms=
sink rate ftmin=

armament1=1 × trainable machine-gun in open position in bow
armament2=Bombs
armament3=
armament4=
armament5=
armament6=
aircontent
see also=
related=
similar aircraft=
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References

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