Amiot 110

__NOTOC__ The Amiot 110, also known as the Amiot-SECM 110, was a French prototype interceptor designed and built in 1929.

Development

The 110 was designed as a contender in the so-called "Jockey" lightweight interceptor contest in which it competed against 9 other types. It was of all-metal construction, with fabric wing skinning. Basically a parasol monoplane, it was fitted with a jettisonable aerofoil-section fuel tank inserted in the fuselage aft of the main undercarriage.

Operational history

It first flew in June 1928, and looked a promising candidate to win the "Jockey" contest. However, it crashed on 1 July 1929 due to several loose rivets and integrity flaws, and no further production went ahead.

pecifications

aerospecs
ref=
met or eng?=met

crew=1
capacity=
length m=6.50
length ft=21
length in=4
span m=10.50
span ft=34
span in=5⅓
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=2.83
height ft=9
height in=2¼
wing area sqm=21.00
wing area sqft=226.05
swept area sqm=
swept area sqft=
rot area sqm=
rot area sqft=
volume m3=
volume ft3=
aspect ratio=
wing profile=
empty weight kg=1120
empty weight lb=2469
gross weight kg=1500
gross weight lb=3307
lift kg=
lift lb=

eng1 number=1
eng1 type=Hispano-Suiza 12Mb 12-cylinder liquid cooled engine
eng1 kw=373
eng1 hp=500
eng1 kn=
eng1 lbf=
eng1 kn-ab=
eng1 lbf-ab=
eng2 number=
eng2 type=
eng2 kw=
eng2 hp=
eng2 kn=
eng2 lbf=
eng2 kn-ab=
eng2 lbf-ab=

max speed kmh=296
max speed mph=184
max speed mach=
cruise speed kmh=
cruise speed mph=
range km=500
range miles=310
endurance h=
endurance min=
ceiling m=
ceiling ft=
glide ratio=
climb rate ms=
climb rate ftmin=
sink rate ms=
sink rate ftmin=

armament1=2 x .303 Vickers machine guns
armament2=
armament3=
armament4=
armament5=
armament6=

References

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