Klemm Kl 105

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The Klemm Kl 105 was a two-seat sport aircraft developed in Germany in 1938. It was a low-wing cantilever monoplane of conventional design with fixed, tailskid undercarriage, and side-by-side seating for two within an enclosed cockpit. Construction throughout was of wood, with the fuselage built using a new semi-monocoque technique which Klemm patented. Plans to produce the design in series were abandoned with the outbreak of the Second World War.

pecifications

aerospecs
ref=
met or eng?= met

crew=One pilot
capacity=1 passenger
length m=7.35
length ft=24
length in=1
span m=10.92
span ft=35
span in=10
swept m=
swept ft=
swept in=
rot number=
rot dia m=
rot dia ft=
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dia m=
dia ft=
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width m=
width ft=
width in=
height m=2.00
height ft=6
height in=7
wing area sqm=15.00
wing area sqft=161
swept area sqm=
swept area sqft=
rot area sqm=
rot area sqft=
volume m3=
volume ft3=
aspect ratio=
wing profile=
empty weight kg=340
empty weight lb=750
gross weight kg=560
gross weight lb=1,230
lift kg=
lift lb=

eng1 number=1
eng1 type=Zündapp Z 9
eng1 kw= 37
eng1 hp= 50
eng1 kn=
eng1 lbf=
eng1 kn-ab=
eng1 lbf-ab=
eng2 number=
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eng2 kw=
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max speed kmh=150
max speed mph=90
max speed mach=
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stall speed kmh=
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range km=500
range miles=310
endurance h=
endurance min=
ceiling m=3,000
ceiling ft=9,800
g limits=
roll rate=
glide ratio=
climb rate ms=1.8
climb rate ftmin=350
sink rate ms=
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armament6= aircontent
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References

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