Aerospace Engines A to Z
Aerospace Engines A to Z

Updated: 26-Oct-2020

This is one of the heirs of Nakajima, an important aeronautical construction company of WWII.

-Omiya-Fuji Kogyo Kabushiki Kaisha, made the JO-1 axial flow turbojet destined for an aircraft of the Armed Forces of Defense.

-The JO-1 has an 8-stage compressor, eight combustion chambers and a single turbine. It delivered 2205 lbs of thrust at 12,000 rpm.

From Appendix A4/6: The JO-1 turbojet engine mentioned in the main text may clearly be a development of the Ne-20 but Americanized, in the style of the J-35 and J-47, with visible separate combustion chambers.

-Photo of the prototype with the company's president. Omija is a division of Fuji Heavy Industries.

Mr. Kita Kenji and the JO-1
"Mr. Kita Kenji and the JO-1"

Esquema del OMIYA JO-1
“Esquema del JO-1”

Engines of OMIYA FUJI

Model: JO-1

Arquitecture:
Compressor/s: 8-stage axial compressor
Combustion chambers: 8 combustion chambers
Turbines: Single stage turbine
Power / Thrust: --- / 2205 Lbf
Weight:

Other details: