Ace K-1

The Ace K-1 was a United States single-seat biplane aircraft designed in 1919 by Alexander Klemin, then Professor of Aeronautical Engineering at New York University (NYU). Later versions included a nearly faired-in engine installation and some were fitted with the Salmson AD-9 engine.

pecifications (K-1)

aircraft specifications
plane or copter?=plane
jet or prop?=prop
ref=
crew=one pilot
capacity=
payload main=
payload alt=
length main= 18 ft 0 in
length alt= 5.49 m
span main= 28 ft 4 in
span alt= 8.64 m
height main=
height alt=
area main=
area alt=
airfoil=
empty weight main=
empty weight alt=
loaded weight main=
loaded weight alt=
useful load main=
useful load alt=
max takeoff weight main=
max takeoff weight alt=
more general=
engine (prop)= inline engine
type of prop=
number of props=1
power main= 40 hp
power alt= 36 kW
power original=
max speed main= 63 mph
max speed alt= 100 km/h
cruise speed main=
cruise speed alt=
stall speed main=
stall speed alt=
never exceed speed main=
never exceed speed alt=
range main= 160 miles
range alt=256 km
ceiling main=
ceiling alt=
climb rate main=
climb rate alt=
loading main=
loading alt=
thrust/weight=
power/mass main=
power/mass alt=
more performance=
armament=
avionics=

ee also

aircontent
related=

similar aircraft=

sequence=

lists=

see also=