Abraham Iris

Infobox Aircraft
infoboxwidth=16
name=Abraham Iris


caption=
manufacturer=Abraham
type=Touring aircraft
designer=
first flight=
introduced=
retired=
status=
primary user=
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produced=1930s
number built=
unit cost=
variants with their own articles=The Abraham Iris was a two-seat touring airplane produced in France in the early 1930s in two slightly different versions, the Iris I with a 75 kW (100 hp) Hispano-Suiza piston engine, and the Iris II with a Renault engine. The Iris was a conventional parasol wing monoplane with a neatly faired-in engine.

pecifications (Iris II)

aircraft specifications

plane or copter?=plane
jet or prop?=prop

crew=1
capacity=1 passenger
length alt=22 ft 6 in
length main=6.87 m
span alt=32 ft 2 in
span main=9.80 m
height alt=7 ft 7 in
height main=2.50 m
area alt=161 ft²
area main=15 m²
empty weight alt=1,027 lb
empty weight main=467 kg
loaded weight alt=1,672 lb
loaded weight main=760 kg
max takeoff weight alt=
max takeoff weight main=

engine (prop)=
type of prop=Renault 4Pb
number of props=1
power alt=95 hp
power main=71 kW

max speed alt=98 knots, 113 mph
max speed main=180 km/h
range alt=220 nm, 250 mi
range main=400 km
ceiling alt=
ceiling main=
climb rate alt=
climb rate main=
loading alt=10 lb/ft²
loading main=51 kg/m²
power/mass alt=0.06 hp/lb
power/mass main=90 W/kg

ee also

aircontent

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* List of utility aircraft