The early development of aircraft in Japan was fully dependent on engines from abroad, although many of these designs were license built by Japanese companies.
Gasuden was no exception, building
Le Rhone rotaries in the early 1920s. However, by 1926, the company had gained enough experience to develop its own first engine. Taking inspiration from the
Armstrong Siddeley Mongoose, the company developed a seven-cylinder star-shaped radial made of alloy and using an integral impellor-based carburettor. The prototype was first run in 1927 and was the first indigenous design to achieve production in Japan. The resulting engine was a single row radial with seven cylinders of bore and stroke . Running on
80 Octane fuel, the engine was rated at sea level at . The engine had no
compressor, although some later models were fitted with a single speed mechanical
supercharger to boost performance. Initially, the engine was first known as the , but was later better known as the as the range of engines produced by the company increased. Production ran from 1928 to 1944. Large numbers were delivered, primarily for training and other light aircraft. Amongst the more numerous were the Yokosuka K2Y2 Type 3, a derivative of the
Avro 504N which was produced from 1929 to 1940, and the
Yokosuka K4Y1 seaplane produced between 1933 and 1940, mainly by
Watanabe. In May 1939, Hitachi acquired Tokyo Gas and Electric Company, merging the aeronautical part of the business with Hitachi Aircraft. The engine was rebranded Hitachi. Production totalled between 8,300 and 12,500 units. ==Variants==