<?xml version="1.0"?>
<!-- turbofan engine model from Stevens simualtion text -->
<FG_TURBINE NAME="low_bypass_turbofan">
  <!-- max military thrust (no afterburner), lbs -->
  MAXMILTHRUST 12680
  <!-- max augmented thrust (afterburner lit), lbs -->
  MAXAUGTHRUST 28886
  <!-- Idle Thrust -->
  <TABLE NAME="IdleThrust" TYPE="TABLE">
    Idle_power_thrust
    6
    6
    velocities/mach-norm
    position/h-sl-ft
    none
                0   10000   20000   30000   40000  50000
    0.0    0.0836  0.0528  0.0694  0.0899  0.1183  0.1467
    0.2    0.0501  0.0335  0.0544  0.0797  0.1049  0.1341
    0.4    0.0047  0.0020  0.0272  0.0595  0.0891  0.1203
    0.6   -0.0804 -0.0560 -0.0237  0.0276  0.0718  0.1073
    0.8   -0.2129 -0.1498 -0.1025 -0.0195  0.0473  0.0868
    1.0   -0.2839 -0.1104 -0.0469 -0.0270 -0.0158  0.0552
  </TABLE>

  <TABLE NAME="MilThrust" TYPE="TABLE">
    Military_power_thrust
    6
    6
    velocities/mach-norm
    position/h-sl-ft
    none
               0    10000   20000     30000    40000    50000
    0.0   1.0000   0.7216   0.4890   0.3115   0.1932   0.1104
    0.2   1.0000   0.7216   0.4979   0.3186   0.1948   0.1104
    0.4   0.9945   0.7344   0.5213   0.3383   0.2050   0.1230
    0.6   0.9968   0.7759   0.5591   0.3675   0.2240   0.1309
    0.8   0.9771   0.8025   0.6112   0.4196   0.2563   0.1522
    1.0   0.9211   0.7767   0.6349   0.4811   0.2997   0.1822
  </TABLE>

  <TABLE NAME="AugThrust" TYPE="TABLE">
    Augmented_thrust
    6
    6
    velocities/mach-norm
    position/h-sl-ft
    none
                0    10000   20000     30000    40000    50000
    0.0    0.6924   0.5193   0.3739   0.2423   0.1385   0.0865
    0.2    0.7415   0.5435   0.3886   0.2535   0.1535   0.0900
    0.4    0.7858   0.5837   0.4241   0.2823   0.1731   0.0981
    0.6    0.8392   0.6546   0.4764   0.3214   0.1973   0.1113
    0.8    0.9025   0.7296   0.5530   0.3848   0.2375   0.1367
    1.0    1.0000   0.8073   0.6335   0.4668   0.2992   0.1751
  </TABLE>
</FG_TURBINE>