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K11W Shiragiku, Japanese Trainer Aircraft


Photograph of K11W Shiragiku in surrender colors

Wikipedia Commons


Kyushu K11W Shiragiku ("White Chrysanthemum")


Specifications:


Crew
5
Dimensions 49'3" by 33'8" by 12'11"
14.98m by 10.24m by 3.93m
Weight 3697-6173 lbs
1677-2800 kg
Speed 143 mph at 5580 feet
230 km/h at 1700 meters
Cruising speed       109 mph at 3280 feet
175 km/h at 1000 meters
Climb rate 8.4 feet per second
2.6 meters per second
Ceiling 18,440 feet
5620 meters
Power plant One 515 hp (384 kW) Hitachi GK2B Amakaze 21 nine-cylinder air-cooled radial engine driving a two-bladed metal propeller.
Armament 1 rear-firing flexible 7.7mm Type 92 machine gun
External stores 2 30kg (66lb) bombs
1 250 kg (551lb) bomb as kamikaze
Range 1093 miles
1759 km
Production A total of 798 aircraft (1942-11 to 1945-8)
Variants

The K11W2 was an all-wood version built in small numbers.

The Q3W1 Nankai ("South Seas") was a two-seat antisubmarine version that failed to reach production after the prototype made a belly landing.


The K11W Shiraguki was a trainer for bomber crewmen with a rather unusual configuration. The pilot and radio operator/gunner sat in a greenhouse canopy above the wing while the instructor, navigator, and bombardier were in a cabin located under the wing.

The design originated in 1940 at Watanabe Tekkosho K.K. as a replacement for the K3M. The design resembled the American O-47. The prototype made its first flight in November 1942 and proceeded rapidly into production as no significant bugs were encountered. However, by the time production started, Watanabe Tekkosho had been absorbed into Kyushu Hikoki K.K.

References

Francillon (1979)



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