The Japanese Army found
itself faced with the prospect of 275 Ki-61-II airframes sitting around
waiting for installation of their Ha-140 liquid-cooled engines. The
Ha-140 engine had proven to be totally unreliable and to make matters
worse, the factory manufacturing the Ha-140 had been destroyed in a
B-29 raid. Since Japan desperately needed aircraft capable of
intercepting the B-29's, in November of 1944 the Ministry of Munitions
instructed Kawasaki to install a different powerplant in the Ki-61-II
in an attempt to get as many aircraft in the air as possible.
Kawasaki Ki-100-Ia of the 3rd Chutai, 18th Sentai operating from
Kashiwa in the spring of 1945
After testing the
available engines, Kawasaki finally settled on the 1500 hp Mitsubishi
Ha-112-II fourteen-cylinder double-row radial engine. This engine had
established a standard of easy maintenance and reliable service, which
contrasted markedly with the notoriously unreliable and temperamental
Ha-140. However, the Ha-112 was a radial engine, and, with a diameter
of four feet, the installation of this engine in a fuselage only 33
inches wide provided a major challenge. However, the Kawasaki concern
was guided in its work by being able to study the engine mount in an
imported Focke-Wulf Fw 190A, an example in which a wide radial engine
had been successfully installed in an airframe with a narrow width. In
addition, the same Mitsubishi Ha-112 radial engine had been
successfully installed in the Aichi-built D4Y3 (Allied code name JUDY)
dive bomber, earlier versions of which had been powered by a
liquid-cooled engine.
The new project was
sufficiently different from the Ki-61 Hien that it was assigned a new
Kitai number, Ki-100. Three Ki-61-II airframes were experimentally
modified as Ki-100s by the installation of the Ha-112 radial. The first
Ki-100 prototype aircraft made its first flight on February 1, 1945.
The results of the flight testing exceeded everyone's expectations. The
Ki-100 was about 600 pounds lighter than its Ki-61-II predecessor.
Manoeuvrability and handling were markedly improved due to the lower
wing and power loading. Although the maximum speed of the Ki-100 was
slightly lower than that of the Ki-61-II because of the higher drag
exerted by the radial engine, this performance could be reliably
attained because of the better reliability of the Ha-112 engine. The
design was ordered into immediate production as the Army Type 5 Fighter
Model 1A (Ki-100-Ia).
The first Type 5
fighters (Ki-100-Ia) were direct conversions of existing Ki-61-II
airframes. 271 airframes were converted between March and June 1945,
and were immediately delivered to operational units.
The Ki-100 was simple
to fly and maintain. Even the most inexperienced pilots were able to
get the hang of the Ki-100 relatively quickly. The Ha-112 engine proved
to be quite reliable and simple to maintain. In combat, the Ki-100-Ia
proved to be an excellent fighter, especially at low altitudes. It
possessed a definite ascendancy over the Grumman F6F Hellcat. In one
encounter over Okinawa, a Ki-100-equipped unit destroyed 14 F6F Hellcat
fighters without loss to themselves. When the Ki-100 encountered the
P-51D Mustang at low or medium altitudes over Japan, it was able to
meet the American fighter on more or less equal terms. The outcome of
P- 51D vs Ki-100 battles was usually determined by piloting skill or by
numerical advantage rather than by the relative merits of the two
fighter types. However, at altitudes above 26,000 feet, the
manoeuvrability of the Ki-100 began to fall off rather severely and the
fighter was at a relative disadvantage in intercepting the high-flying
B-29.
Even though the Ki-100
was a virtually different aircraft, it was derived from the Ki-61-II
Hien, and as such was never given a seperate codename by the allies.
The Japanese continued to refer to it as the "Hien" but the carryover
of the name was never official, perhaps due to its short time in
service.
By June, 1945, all of
the Ki-61-II airframes had been used up, and further Ki-100s were built
from the outset as radial-powered machines. This version was designated
Ki-100-Ib. The Ki-100-Ib differed from the Ki-100-Ia in having an
all-round vision hood similar to that fitted to the experimental
Ki-61-III. The first Ki-100-Ib fighters were built at the Kagamigahara
and Ichinomiya Kawasaki factories in May of 1945, but production was
severely hampered by the continual Allied bombing. Plans had been made
to produce 200 fighters per month, but the Ichinomiya plant was forced
to shut down in July 1945 after having built only 12 aircraft, and the
Kagamigahara plant had its production severely curtailed by aerial
attacks. By the time of the Japanese surrender, only 118 Ki-100-Ib
aircraft had been delivered.
A Kawasaki Ki-100-Ib of the 3rd Chutai, 59th Sentai
In an attempt to
improve the high-altitude performance, the Ki-100-II version was
evolved. It was powered by a 1500 hp Mitsubishi Ha-112-II Ru with a
turbo supercharger and water-methanol injection to boost power for
short intervals. Because of a lack of space, the turbo supercharger had
to be mounted underneath the engine without provision for an
intercooler and its associated ducting, with air being ducted directly
from the compressor to the carburettor. It first flew in May 1945. The
lack of an intercooler limited the high-altitude performance of the
Ki-100-II, and the turbo supercharger added 600 pounds to the weight,
which reduced maximum speed by 15 mph at 10,000 feet. However, the
boosted high-altitude power enabled a maximum speed of 367 mph to be be
reached at 32,800 feet (the cruising altitude of the B-29 during
daylight operations). It had been planned to begin production of the
Ki-100-II in September of 1945, but only three prototypes of this
high-altitude interceptor had been produced by the time of the Japanese
surrender.
A total of 396 Ki-100s
were built, including 275 Ki-61-II conversions, 118 Ki-100-Ib
production aircraft built from scratch, and three Ki-100-II prototypes.
Most of them were assigned to the defence of the home islands,
operating from Chofu and Yokkaichi from the spring of 1945. At the end
of the war, two Ki-100-Ibs were shipped to the USA for evaluation. Its
presumed they were scrapped in the late 1940s, along with a lot of
other captured Axis aircraft.
(Army Type 5 Fighter
Model 1A - Kawasaki Ki-100-Ia/b Goshiki-Sen "Experimental Fighter")
Allied code: No
separate codename was given, but generally called a Tony
Type: Single
Seat Fighter Interceptor
Powerplant: One
1,500 hp (1119 kw) Mitsubishi Ha-112-II 14-cylinder radial piston
engine.
Performance:
Maximum speed 367 mph (590 km/h) at 32,810 ft (10000 m); cruising speed
217 mph (350 km/h); service ceiling 35,008 ft (10670 m); climb to
32,810 ft (10000 m) in 20 minutes.
Range: 1,243
miles (2000 km) with internal fuel stores.
Weight: Empty
5,952 lbs (2700 kg) with a maximum take-off weight of 8,091 lbs (3670
kg).
Dimensions: Span
39 ft 4 1/2 in (12.00 m); length 28 ft 10 1/2 in (8.80 m); height 12 ft
3 1/2 in (3.75 m); wing area 215.29 sq ft
(20.00 sq m).
Armament: Two
fuselage mounted 12.7 mm (0.50 in) machine guns and two wing mounted 20
mm Ho-5 cannon, plus two drop tanks or two 551 lbs (250 kg) bombs.
Variants:
Ki-100, Ki-100-Ia (Army Type 5 Fighter Model 1A), Ki-100-Ib (cut down
rear fuselage and an all round view canopy), Ki-100-II (three
prototypes). Operators: Japanese Army.