Dual-Spool Turbofan

Aerodynamic visualizer featuring concentric N1/N2 shafts, 24-blade fan, 8-stage HPC compression, and annular combustor.

St 0: INLET

St 2: FAN / LPC

St 3: HPC

St 4: COMBUSTOR

St 5: HPT / LPT

St 7: NOZZLE

Dual-Spool Telemetry

N1 (LP SPOOL) 3,450 RPM

N2 (HP SPOOL) 14,200 RPM

NET THRUST 128.4 kN

T4 COMBUST TEMP 1,720 K

PRESS RATIO (OPR) 38.5 : 1

AIRFLOW RATE 420 kg/s

THROTTLE (N1 / N2)

EXPLODE STAGES