Updated: 18-Jul-2018
This is a Japanese association for jet engine research, jointly with the Japanese government and the following industries:
“FJR-710”
-Kawasaki Heavy Industries Co.
-Mitsubishi Heavy Industries Co.
“FJR-710”
-Between 1971 and 1981, they designed and developed the FJR-710 as a third generation turbofan.
-For the FJR-710-600 model we have a by-pass ratio of 6, and a thrust at take-off of 5,100 Kgf.
-The engine diameter was 1,240 mm with a length of 2,353 mm, and it weighed 980 Kgs.
Engines of ENGINEERING RESEARCH ASSOCIATION
Model: FJR-710
Arquitecture: Turbofan
Compressor/s:
Combustion chambers:
Turbines:
Power / Thrust: --- / 5100 Kgf
Weight:
"Engineering Research Association, FJR-710"