JDM Roitelet

__NOTOC__ Infobox Aircraft
name=Roitelet


caption=
type=Sports aircraft
manufacturer=Homebuilt
designer=
first flight=3 January 1949
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variants with their own articles=The JDM Roitelet (French: "Wren") was a single-seat light aircraft marketed in France by Avions JDM shortly after World War II. However, only a single example (the prototype, registration "F-WFAC") is known to have been built. It was a low-wing, open cockpit monoplane with tailskid undercarriage.

pecifications

aerospecs
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crew=one pilot
capacity=
length m=4.15
length ft=13
length in=7
span m=6.95
span ft=22
span in=10
dia m=
dia ft=
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height m=
height ft=
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wing area sqm=
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aspect ratio=
empty weight kg=105
empty weight lb=230
gross weight kg=210
gross weight lb=460

eng1 number=1
eng1 type=Poinsard piston engine
eng1 kw= 19
eng1 hp= 25
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eng1 lbf=
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max speed kmh=155
max speed mph=97
max speed mach=
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range km=340
range miles=210
endurance h=
endurance min=
ceiling m=
ceiling ft=
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References

*
* [http://www.aviafrance.com/5909.htm aviafrance.com]
* [http://www.luftfahrt-archiv.de/Flugzeugtypen.asp?Type=Link&ID=T1484&SID=167741514 luftfahrt-archiv.de]

ee also

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