Leduc 0.22

Leduc 0.22

__NOTOC__

The Leduc 0.22 was the prototype of a Mach 2 fighter built in France in 1956. It was the first attempt at a practical application of the ramjet technology that had been developed in the 0.10 and 0.21 research aircraft over the previous years. Unlike all previous Leduc aircraft, it featured swept wings and a coaxial turbojet-ramjet powerplant to enable unassisted operation.

Flown since 26 December 1956 on turbojet power alone, the ramjet was finally fired on the 34th flight, on 18 May 1957. Another 80 flights took place before the cancellation of the project in favour of the more conventional Dassault Mirage III. A second prototype was under construction at the time.

Although intended to be a supersonic fighter, the 0.22 proved unable to exceed the speed of sound (Mach 1) because of the prohibitive drag induced by its non-area-ruled fuselage at near-sonic speeds. The cancellation of the project marked the end of René Leduc's aircraft development activities.

pecifications

aerospecs
ref=
met or eng?= met

crew=One pilot
capacity=
length m=18.21
length ft=59
length in=9
span m=9.95
span ft=32
span in=8
swept m=
swept ft=
swept in=
rot number=
rot dia m=
rot dia ft=
rot dia in=
dia m=
dia ft=
dia in=
width m=
width ft=
width in=
height m=
height ft=
height in=
wing area sqm=22.1
wing area sqft=238
swept area sqm=
swept area sqft=
rot area sqm=
rot area sqft=
volume m3=
volume ft3=
aspect ratio=
wing profile=
empty weight kg=6,380
empty weight lb=14,040
gross weight kg=8,995
gross weight lb=19,789
lift kg=
lift lb=

eng1 number=1
eng1 type=Leduc ramjet
eng1 kw=
eng1 hp=
eng1 kn= 63.7
eng1 lbf= 14,300
eng1 kn-ab=
eng1 lbf-ab=
eng2 number=1
eng2 type=SNECMA Atar 101D-3
eng2 kw=
eng2 hp=
eng2 kn= 31.4
eng2 lbf= 7,040
eng2 kn-ab=
eng2 lbf-ab=

max speed kmh=1,200
max speed mph=750
max speed mach=
cruise speed kmh=
cruise speed mph=
stall speed kmh=
stall speed mph=
range km=
range miles=
endurance h=
endurance min=
ceiling m=
ceiling ft=
g limits=
roll rate=
glide ratio=
climb rate ms=
climb rate ftmin=
sink rate ms=
sink rate ftmin=

armament1=
armament2=
armament3=
armament4=
armament5=
armament6= aircontent
see also=
related=
similar aircraft=
lists=

References

*
*

External links

* http://xplanes.free.fr/stato/stato-2.html


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