Brochet MB.120

__NOTOC__ Infobox Aircraft
name=MB.120


caption=
type=Sports plane
manufacturer=Brochet
designer=Maurice Brochet
first flight=5 April 1954
introduced=
retired=
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primary user=
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produced=
number built=1
variants with their own articles=The Brochet MB.120 was a two-seat light aircraft developed in France in the 1950s. It was a further derivative of the Brochet MB.70 family, combining the wing of the MB.80 with a modified version of the MB.100 that had its seating capacity reduced. The design never progressed past a single prototype.

pecifications

aerospecs
met or eng?= met

crew=One pilot
capacity=1 passenger
length m=6.50
length ft=21
length in=4
span m=10.65
span ft=34
span in=11
swept m=
swept ft=
swept in=
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dia m=
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volume m3=
volume ft3=
aspect ratio=
empty weight kg=
empty weight lb=
gross weight kg=765
gross weight lb=1,687
lift kg=
lift lb=

eng1 number=1
eng1 type=Continental C90
eng1 kw= 67
eng1 hp= 90
eng1 kn=
eng1 lbf=
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eng1 lbf-ab=
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max speed kmh=195
max speed mph=122
max speed mach=
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range km=
range miles=
endurance h=
endurance min=
ceiling m=
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armament1=
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References

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ee also

aircontent

related=

similar aircraft=

sequence=
* ← MB.80 - MB.100 - MB.110 - MB.120

lists=

see also=