<?xml version="1.0"?>
<!--
  File:     J85.xml
  Author:   Aero-Matic v 0.8
  Modified for J85-GE-5, Dave Culp

  Inputs:
    name:           J85
    type:           turbine
    thrust:         2050.0 lb
    augmented?      yes
    injected?       no
-->

<turbine_engine name="J85">
  <milthrust>    2050.0 </milthrust>
  <maxthrust>    2900.0 </maxthrust>
  <bypassratio>     0.0 </bypassratio>
  <tsfc>            0.85 </tsfc>
  <atsfc>           1.72 </atsfc>
  <bleed>           0.03 </bleed>
  <idlen1>          0.0 </idlen1>
  <idlen2>         53.0 </idlen2>
  <maxn1>         100.0 </maxn1>
  <maxn2>         100.0 </maxn2>
  <augmented>         1 </augmented>
  <augmethod>         2 </augmethod>
  <injected>          0 </injected>

  <function name="IdleThrust">
   <table>
    <independentVar lookup="row">velocities/mach</independentVar>
    <independentVar lookup="column">atmosphere/density-altitude</independentVar>
    <tableData>
         -10000     0     10000   20000   30000   40000   50000   60000
     0.0  0.0528  0.0488  0.0528  0.0694  0.0899  0.1183  0.1467  0.0
     0.2  0.0600  0.0501  0.0335  0.0544  0.0797  0.1049  0.1342  0.0
     0.4  0.0100  0.0047  0.0020  0.0272  0.0595  0.0891  0.1203  0.0
     0.6 -0.0600 -0.0804 -0.0560 -0.0237  0.0276  0.0718  0.1073  0.0
     0.8 -0.2000 -0.2129 -0.1498 -0.1025 -0.0195  0.0473  0.0868  0.0
     1.0 -0.2300 -0.2839 -0.1104 -0.0469 -0.0270 -0.0158  0.0552  0.0
    </tableData>
   </table>
  </function>

  <function name="MilThrust">
   <table>
    <independentVar lookup="row">velocities/mach</independentVar>
    <independentVar lookup="column">atmosphere/density-altitude</independentVar>
    <tableData>
          -10000       0   10000   20000   30000   40000   50000   60000
     0.0   1.2600  1.0000  0.7400  0.5340  0.3720  0.2410  0.1490  0.0
     0.2   1.1710  0.9340  0.6970  0.5060  0.3550  0.2310  0.1430  0.0
     0.4   1.1500  0.9210  0.6920  0.5060  0.3570  0.2330  0.1450  0.0
     0.6   1.1810  0.9510  0.7210  0.5320  0.3780  0.2480  0.1540  0.0
     0.8   1.2580  1.0200  0.7820  0.5820  0.4170  0.2750  0.1700  0.0
     1.0   1.3690  1.1200  0.8710  0.6510  0.4750  0.3150  0.1950  0.0
     1.2   1.4850  1.2300  0.9750  0.7440  0.5450  0.3640  0.2250  0.0
     1.4   1.5941  1.3400  1.0860  0.8450  0.6280  0.4240  0.2630  0.0
    </tableData>
   </table>
  </function>

  <function name="AugThrust">
   <table>
    <independentVar lookup="row">velocities/mach</independentVar>
    <independentVar lookup="column">atmosphere/density-altitude</independentVar>
    <tableData>
           -10000       0   10000   20000   30000   40000   50000   60000
     0.0    1.1816  1.0000  0.8184  0.6627  0.5280  0.3756  0.2327  0.0
     0.2    1.1308  0.9599  0.7890  0.6406  0.5116  0.3645  0.2258  0.0
     0.4    1.1150  0.9474  0.7798  0.6340  0.5070  0.3615  0.2240  0.0
     0.6    1.1284  0.9589  0.7894  0.6420  0.5134  0.3661  0.2268  0.0
     0.8    1.1707  0.9942  0.8177  0.6647  0.5309  0.3784  0.2345  0.0
     1.0    1.2411  1.0529  0.8648  0.7017  0.5596  0.3983  0.2467  0.0
     1.2    1.3287  1.1254  0.9221  0.7462  0.5936  0.4219  0.2614  0.0
     1.4    1.4365  1.2149  0.9933  0.8021  0.6360  0.4509  0.2794  0.0
     1.6    1.5711  1.3260  1.0809  0.8700  0.6874  0.4860  0.3011  0.0
     1.8    1.7301  1.4579  1.1857  0.9512  0.7495  0.5289  0.3277  0.0
     2.0    1.8314  1.5700  1.3086  1.0474  0.8216  0.5786  0.3585  0.0
     2.2    1.9700  1.6900  1.4100  1.2400  0.9100  0.6359  0.3940  0.0
     2.4    2.0700  1.8000  1.5300  1.3400  1.0000  0.7200  0.4600  0.0
     2.6    2.2000  1.9200  1.6400  1.4400  1.1000  0.8000  0.5200  0.0
    </tableData>
   </table>
  </function>

</turbine_engine>
