BR700-710A2-20

BR700-710A2-20 is a turbofan engine model used in aircraft.

Specifications

Engine Family: turbofan

Bypass ratio: 3.8

Control system: FADEC

Dry weight: 1891 kilogram

Fan diameter: 1.22 metre

Fan stages: 1

HP compressor stages: 10

HP turbine stages: 2

LP turbine stages: 2

Length: 4.67 metre

Max. continuous thrust: 64.3 kilonewton

Max. takeoff thrust: 65.6 kilonewton

N1 RPM: 7431

N2 RPM: 15898