The Kawanishi K6K was a two-seat, twin-float biplane trainer built by the Kawanishi Aircraft Company in the late 1930s as a prototype for the Imperial Japanese Navy. It was conceived to meet a Navy requirement for an intermediate-level training seaplane and used a welded steel-tube fuselage covered in fabric, a fabric-covered steel wing and light alloy monocoque floats. Power came from a single Nakajima Kotobuki 9-cylinder air-cooled radial engine. Its first flight took place on 30 April 1938, but the flight tests revealed poor alighting characteristics, so the type was not ordered into production and only two prototypes were completed.
Facts
Engine Class Top Speed (km/h) Comparison
Body StyleAircraft (no road body style) 1 Connections
Exemplifies
Source Kawanishi K6K (Wikipedia)
Of Make
Source Kawanishi K6K (Wikipedia)
In the Other Atlases
Manufactured By
Also in Business Atlas: the manufacturer of this subject.
Source Kawanishi K6K (Wikipedia)Lead, manufacturerQuote, Lead, manufacturer
built by the Kawanishi Aircraft Company
Originated In
Also in Geography Atlas: where this subject originated.
Source Kawanishi K6K (Wikipedia)LeadQuote, Lead
prototype Japanese training aircraft
Sources
1. Kawanishi K6K (Wikipedia)
Lead
prototype Japanese training aircraft
Lead, status
was a prototype Japanese training aircraft
Design
The first flight of the K6K occurred on 30 April 1938
Specifications
9-cylinder air-cooled radial piston engine
Specifications, mass
Empty weight: 1,300 kg
Specifications, top speed
Maximum speed: 232 km/h
Lead, manufacturer
built by the Kawanishi Aircraft Company
View the SourceReader Challenges (0)
No disputes yet. Spotted an error or a better source? Open the first one.
Sign in to dispute this or suggest a correction.