<?xml version="1.0"?>
<!--
  File:     CF6-80C2.xml
  Author:   Aero-Matic v 0.7

  Inputs:
    name:           CF6-80C2
    type:           turbine
    thrust:         184500 lb
    augmented?      no
    injected?       no
-->

<FG_SIMTURBINE NAME="CF6-80C2">
  MILTHRUST 184500
  MAXTHRUST 184500
  BYPASSRATIO    1.0
  TSFC           0.8
  ATSFC          1.7
  IDLEN1        30.0
  IDLEN2        60.0
  MAXN1        100.0
  MAXN2        100.0
  AUGMENTED      0
  AUGMETHOD      1
  INJECTED       0

<TABLE NAME="IdleThrust" TYPE="TABLE">
  Idle_power_thrust_factor
  6
  7
  velocities/mach-norm
  position/h-sl-ft
  none
       -10000     0     10000   20000   30000   40000   50000
  0.0  0.0430  0.0488  0.0528  0.0694  0.0899  0.1183  0.1467
  0.2  0.0500  0.0501  0.0335  0.0544  0.0797  0.1049  0.1342
  0.4  0.0040  0.0047  0.0020  0.0272  0.0595  0.0891  0.1203
  0.6  0.0     0.0     0.0     0.0     0.0276  0.0718  0.1073
  0.8  0.0     0.0     0.0     0.0     0.0474  0.0868  0.0900
  1.0  0.0     0.0     0.0     0.0     0.0     0.0552  0.0800
</TABLE>

<TABLE NAME="MilThrust" TYPE="TABLE">
  Military_power_thrust_factor
  8
  7
  velocities/mach-norm
  position/h-sl-ft
  none
        -10000       0   10000   20000   30000   40000   50000
  0.0   1.2600  1.0000  0.7400  0.5340  0.3720  0.2410  0.1490
  0.2   1.1710  0.9340  0.6970  0.5060  0.3550  0.2310  0.1430
  0.4   1.1500  0.9210  0.6920  0.5060  0.3570  0.2330  0.1450
  0.6   1.1810  0.9510  0.7210  0.5320  0.3780  0.2480  0.1540
  0.8   1.2580  1.0200  0.7820  0.5820  0.4170  0.2750  0.1700
  1.0   1.3690  1.1200  0.8710  0.6510  0.4750  0.3150  0.1950
  1.2   1.4850  1.2300  0.9750  0.7440  0.5450  0.3640  0.2250
  1.4   1.5941  1.3400  1.0860  0.8450  0.6280  0.4240  0.2630
</TABLE>

</FG_SIMTURBINE>