- Glasflügel 206
__NOTOC__ Infobox Aircraft
name=206 Hornet
caption=
type=Standard Class sailplane
national origin=Germany
manufacturer=Glasflügel
designer=Eugen Hanle
first flight=21 December avyear|1974
introduced=
retired=
status=
primary user=
more users=
produced=
number built=102
variants with their own articles=The Glasflügel 206 Hornet was a Standard Class sailplane produced in Germany in the 1970s and 80s. Of conventional sailplane design with a T-tail, it was developed from the Club Libelle and featured the same composite construction throughout. Differences from the earlier aircraft included a redesigned canopy, retractable monowheellanding gear , and provision for 75 kg (165 lb) ofwater ballast .An improved version, the Hornet C was produced in 1979, incorporating a new one-piece canopy originally designed for the Mosquito and an increase in water ballast capacity to 170 kg (375 lb). The wing was also revised, making extensive use of carbon fibre structures to save weight.
pecifications (206)
aerospecs
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met or eng?= metcrew=One pilot
capacity=
length m=6.40
length ft=21
length in=0
span m=15.00
span ft=49
span in=3
swept m=
swept ft=
swept in=
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rot dia m=
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rot dia in=
dia m=
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width m=
width ft=
width in=
height m=1.40
height ft=4
height in=7
wing area sqm=9.8
wing area sqft=106
swept area sqm=
swept area sqft=
rot area sqm=
rot area sqft=
volume m3=
volume ft3=
aspect ratio= 23
empty weight kg=227
empty weight lb=500
gross weight kg=926
gross weight lb=420
lift kg=
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eng2 number=
eng2 type=
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eng2 lbf-ab=max speed kmh=250
max speed mph=155
max speed mach=
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range km=
range miles=
endurance h=
endurance min=
ceiling m=
ceiling ft=
glide ratio= 38
climb rate ms=0.6
climb rate ftmin=119
sink rate ms=
sink rate ftmin=armament1=
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armament6=aircontent
see also=
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lists=References
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