HAT LS2

HAT LS2 (designation standing for "Landplane, Single engine, 2-seater) is a light airplane developed by Hellenic Aeronautical Technologies (HAT), a small Greek manufacturer of aerospace components. Design started in 1990 followed by prototype construction. After a temporary delay of the program, first flight of prototype (SX-LS2) was made on May 23, 1997. Air-worthiness certificate was awarded on September 2, 1999. The plane is a light two-seater sporting airplane constructed of fiber-reinforced composites. Commercially it is available in the form of construction plans.

pecifications (LS2)

aircraft specifications
plane or copter?=plane
jet or prop?=prop
ref=
crew= one, pilot
capacity=two
payload main=
payload alt=
length main= 5.58 m
length alt= 18 ft 3 in
span main= 8.20 m
span alt= 26 ft 10 in
height main= 1.96 m
height alt= 6 ft 5 in
area main= 8.0 m²
area alt= 86.1 ft²
airfoil=
empty weight main= 307 kg
empty weight alt= 677 lb
loaded weight main= 510 kg
loaded weight alt= 1,124 lb
useful load main=
useful load alt=
max takeoff weight main= 534kg
max takeoff weight alt= 1,177 lb
more general=
engine (prop)= Volkswagen
type of prop=
number of props=1
power main= 47.7 kW
power alt= 64 hp
power original=
max speed main=233 km/h
max speed alt= 145 mph
cruise speed main=
cruise speed alt=
stall speed main=
stall speed alt=
never exceed speed main=
never exceed speed alt=
range main=1,046 km
range alt=564 miles
ceiling main=
ceiling alt=
climb rate main= 213 m/min
climb rate alt= 700 ft/min
loading main=66.8 kg/m²
loading alt=13.7 lb/ft²
thrust/weight=
power/mass main=89.4 W/kg
power/mass alt=0.055 hp/lb
more performance=