CARMAM 15-38

__NOTOC__ Infobox Aircraft
name=15-38


caption=
type=Standard Class sailplane
manufacturer=CARMAM
designer=
first flight=17 June 1979
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The CARMAM 15-38 was a French sailplane built in the late 1970s. It utilised the wing design of the CARMAM Aiglon but had an all-new fuselage. Like the Aiglon, this was of fibreglass construction throughout. The 15-38 was easily distinguished from its predecessor by a more streamlined nose and a T-tail.

pecifications

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crew=One pilot
capacity=
length m=6.70
length ft=22
length in=0
span m=15.00
span ft=49
span in=3
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width m=
width ft=
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height m=1.45
height ft=4
height in=9
wing area sqm=11.0
wing area sqft=118
swept area sqm=
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volume m3=
volume ft3=
aspect ratio= 20.6
empty weight kg=230
empty weight lb=507
gross weight kg=440
gross weight lb=970
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max speed kmh=219
max speed mph=136
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glide ratio= 38:1
climb rate ms=
climb rate ftmin=
sink rate ms= 0.6
sink rate ftmin= 118

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References

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ee also

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