LIBIS KB-11

LIBIS KB-11

Infobox Aircraft
name= KB-11 Branko


caption=
type= Four-seat light trainer and tourer
manufacturer=
designer= Letalski Institut Branko Ivanus Solvenija
first flight= 1959
introduced=
retired=
status=
primary user=
more users=
produced=
number built=
variants with their own articles=

The LIBIS KB-11 Branko was a 1950s Yugoslavian four-seat monoplane designed by Letalski Institut Branko Ivanus Solvenija.

Design and development

The aircraft design office of the Letalski Institut Branko Ivanus Solvenija brought together teachers and students of the Ljubljana technical high school. The KB-11 Branko was a development of the earlier two-seat KB-6 Matajur.First flown in December 1959 the KB-11 was a cantilever low-wing monoplane with retractable tricycle landing gear and an enclosed heated and ventilated cockpit for four persons. Intended for use as an air-taxi our business use but only small numbers were built.

pecifications (KB-11)

aerospecs
met or eng?= met

crew=
capacity=Four
length m=
length ft=
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span m=
span ft=
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swept m=
swept ft=
swept in=
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rot dia m=
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dia m=
dia ft=
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width m=
width ft=
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height m=
height ft=
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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=
gross weight lb=
lift kg=
lift lb=

eng1 number=1
eng1 type=Avco Lycoming O-435-1 flat-six piston
eng1 kw= 185
eng1 hp= 134
eng1 kn=
eng1 lbf=
eng1 kn-ab=
eng1 lbf-ab=
eng2 number=
eng2 type=
eng2 kw=
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max speed kmh=245
max speed mph=152
max speed mach=
cruise speed kmh=
cruise speed mph=
range km=950
range miles=590
endurance h=
endurance min=
ceiling m=
ceiling ft=
glide ratio=
climb rate ms=
climb rate ftmin=
sink rate ms=
sink rate ftmin=

armament1=
armament2=
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References

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External links

ee also

aircontent

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