Aero A.102

Infobox Aircraft
infoboxwidth=16
name=Aero A.102


caption=
type=Fighter aircraft
manufacturer=Aero Vodochody
designer=
first flight=1934
introduced=n/a
retired=
status=
primary user=Czech Air Force
more users=
produced=
number built=
unit cost=
variants with their own articles=The Aero A.102 was a Czechoslovakian fighter aircraft that flew in prototype form in 1934. It was developed in response to a Czech Air Force requirement of that year, but was passed over in favour of the Avia B.35.

The A.102 was of gull winged monoplane configuration with tailwheel undercarriage, and was perhaps inspired by the successful PZL P.11.

pecifications (A.102)

aircraft specifications

plane or copter?=plane
jet or prop?=prop
crew=1
length main=7.30 m
length alt=23 ft 11 in
span main=11.50 m
span alt=37 ft 9 in
height main= m
height alt= ft in
area main=18.50 m²
area alt=199 ft²
empty weight main=1,478 kg
empty weight alt=3,252 lb
loaded weight main=2,036 kg
loaded weight alt=4,479 lb
max takeoff weight main= kg
max takeoff weight alt= lb

number of props=1
engine (prop)=Walter-built Gnome-Rhône Mistral Major
type of prop=14Kfs
power alt=670 kW
power main=900 hp

max speed main=434 km/h
max speed alt=234 knots, 271 mph
range main=670 km
range alt=360 nm, 420 mi
ceiling main=10,000 m
ceiling alt=33,000 ft
climb rate main=14.5 m/s
climb rate alt=2,850 ft/min
loading main=110 kg/m²
loading alt=22 lb/ft²
power/mass main=330 W/kg
power/mass alt=0.20 hp/lb

guns=2× forward-firing 7.92 mm (0.312 in) machine guns

ee also

aircontent

similar aircraft=
* PZL P.11

lists=
* List of fighter aircraft