Tachikawa Ki-94

Infobox Aircraft
name = Ki-94


caption =
type = Fighter
national origin = Japan
manufacturer = Tachikawa Aircraft Company Ltd
designer =
first flight =
introduction =
retired =
status = Prototype
primary user =
more users =
produced =
number built = 1
program cost =
unit cost =
developed from =
variants with their own articles = The term Tachikawa Ki-94 refers to two designs of the Tachikawa Hikoki K.K. aircraft factory. The first was a twin-boom monoplane with two engines driving four blade tractor and pusher propellors, but this design was abandoned as being judged too complex by the technical department of the Japanese Air Force [Francillon 1979, p. 265.] . The second Ki-94 design was a more conventional single-seat, piston-engined monoplane fighter, developed for the Army. Intended as a counter to B-29 raids, it was optimized for high-altitude interception with a pressurized cockpit and heavy armament.

One aircraft was completed in August 1945 but before it flew, the war ended.

pecifications (Ki-94-II (estimated performance))

aircraft specifications

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

ref={Virtual Aviation Museum}

crew=1
capacity=
length main= 12 m
length alt= 39 ft 4 in
span main= 14 m
span alt= 45 ft 11 in
height main= 4.65 m
height alt= 15 ft 3 in
area main= 28 m²
area alt= 301 ft²
airfoil=
empty weight main= 4,690 kg
empty weight alt= 10,337 lb
loaded weight main= kg
loaded weight alt= lb
useful load main= kg
useful load alt= kg
max takeoff weight main= 6,450 kg
max takeoff weight alt= 14,216 lb
more general=

engine (prop)= Nakajima Ha-44 12
type of prop= 18 cylinder air cooled radial engine
number of props= 1
power main= 1,835 kW
power alt= 2,461 hp
power original=

max speed main= 712 km/h
max speed alt= 385 knots, 443 mph
cruise speed main= 440 km/h
cruise speed alt= 237 knots, 273 mph
stall speed main=
stall speed alt=