

The Kawasaki Ki-88 was a proposed design that was inspired by the Bell P-39 Airacobra of the US Army Air Forces. It had its liquid-cooled engine mounted behind the cockpit and driving a tractor propeller via an extension shaft. Design was undertaken in 1942 but, following the inspection of a full-scale mockup, development was discontinued within a year as its calculated maximum speed was only slightly higher than that of the Ki-61 already in production.
Kawasaki Ki.88
Type: Fighter
Service: Japanese Army Air Force (JAAF)
Crew: Pilot
Armament: 37mm cannon in the propeller shaft
two 20mm cannons in the lower nose
Reference: Francillon: 483
Specifications:
Length: 33' 5.5" (10.2 m)
Height: n/a
Wingspan: 40' 8.2" (12.4 m)
Wing area: n/a
Empty Weight: n/a
Loaded Weight: 8598 lbs (3900 kg)
Max Weight: n/a
Propulsion:
No. of Engines: 1
Powerplant: Kawasaki Ha-140 liquid-cooled engine
Horsepower: 1500 hp
Performance:
Range (normal): n/a
Cruise Speed: n/a
Max Speed: 373 mph (592 km/h) at 19,685 ft
Climb to/in: n/a
Ceiling: n/a
Production: none made
Additional information on this aircraft can be
found at Wikipedia
HERE.
(go to Kawasaki page)
If you don't see the table of contents at the left of your screen, CLICK HERE to see the rest of this website!