TJ100C-125 is a turbojet engine model used in aircraft.
Engine Family: turbojet
Control system: Single-channel ECU
Dry weight: 19 kilogram
HP compressor stages: 1
HP turbine stages: 1
Height: 0.27 metre
Length: 1.02 metre
Max. continuous thrust: 10 kilonewton
Max. thrust: 12.5 kilonewton
N1 RPM: 60000
Width: 0.27 metre
