In 1934, the Japanese Navy began development of an 18-cylinder, W-type engine known as the 671 kW (900 shp) Model 94, likely a derivative of the French Lorraine aircraft engine. Later, more powerful versions of this engine were undertaken, including the YE2A, which started development around 1937-38.

The YE2A was designed for remote installation within an aircraft fuselage, the purpose being aircraft streamlining and speed. Designed for a pusher installation, the engine was experimentally tested, but probably never test flown.

This Nakajima engine resembles the YE2A, but was designed for tractor installation. It also resembles a version of a Hispano-Suiza engine, which had been studied by the Yokosuka Naval Air Arsenal. Mitsubishi had acquired a license in 1935 for Hispano-Suiza engines, further suggesting how the Japanese might have acquired these engines. The intended airframe application for the engine is unknown.

Along with other Japanese engines, this artifact was collected for the purpose of technical evaluation.

Display Status

This object is not on display at the National Air and Space Museum. It is either on loan or in storage.

Object Details
Date Circa World War II Country of Origin Japan Type PROPULSION-Reciprocating & Rotary Manufacturer Nakajima Hikoki K. K.
Physical Description Type: Reciprocating, 18 cylinders, W-type, liquid cooled, supercharged Power rating: 1,491 kW (2,000 hp) at (Unknown) rpm Displacement: 51.1 L (3,116 cu in.) Bore and Stroke: 146 mm (5.74 in.) x 170 mm (6.69 in.) Weight: 431 kg (950 lb) Dimensions 3-D: 223.5 × 97.2 × 121.9cm (7 ft. 4 in. × 3 ft. 2 1/4 in. × 4 ft.)
Storage (Stand): 8 1/4 × 4 ft. (244.5 × 121.9cm)
3-D: 430.9kg (950lb.)
Materials Aluminum Alloys
Ferrous Alloys
Copper Alloys
Adhesive Tape
Plastics
Wood
Paper
Adhesive
Inventory Number A19670127000 Credit Line Believed to have been transferred from the U.S. Army Air Forces, Wright Field, Dayton, Ohio Data Source National Air and Space Museum Restrictions & Rights Usage conditions apply
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