59 lines
2.1 KiB
XML
59 lines
2.1 KiB
XML
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<?xml version="1.0"?>
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<!-- J85-GE-5 afterburning turbojet engine model -->
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<FG_TURBINE NAME="J85">
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<!-- max static thrust at S.L. (installed), lbs -->
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MAXMILTHRUST 2050
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<!-- max augmented thrust at S.L. (installed), lbs -->
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MAXAUGTHRUST 2900
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<!-- Idle Thrust -->
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<TABLE NAME="IdleThrust" TYPE="TABLE">
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Idle_power_thrust_factor
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6
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6
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velocities/mach-norm
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position/h-sl-ft
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none
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0 10000 20000 30000 40000 50000
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0.0 0.0836 0.0528 0.0694 0.0899 0.1183 0.1467
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0.2 0.0501 0.0335 0.0544 0.0797 0.1049 0.1341
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0.4 0.0047 0.0020 0.0272 0.0595 0.0891 0.1203
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0.6 -0.0804 -0.0560 -0.0237 0.0276 0.0718 0.1073
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0.8 -0.2129 -0.1498 -0.1025 -0.0195 0.0473 0.0868
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1.0 -0.2839 -0.1104 -0.0469 -0.0270 -0.0158 0.0552
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</TABLE>
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<TABLE NAME="MilThrust" TYPE="TABLE">
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Military_power_thrust_factor
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6
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6
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velocities/mach-norm
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position/h-sl-ft
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none
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0 10000 20000 30000 40000 50000
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0.0 1.0000 0.7216 0.4890 0.3115 0.1932 0.1104
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0.2 1.0000 0.7216 0.4979 0.3186 0.1948 0.1104
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0.4 0.9945 0.7344 0.5213 0.3383 0.2050 0.1230
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0.6 0.9968 0.7759 0.5591 0.3675 0.2240 0.1309
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0.8 0.9771 0.8025 0.6112 0.4196 0.2563 0.1522
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1.0 0.9211 0.7767 0.6349 0.4811 0.2997 0.1822
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</TABLE>
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<TABLE NAME="AugThrust" TYPE="TABLE">
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Augmented_thrust
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8
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6
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velocities/mach-norm
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position/h-sl-ft
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none
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0 10000 20000 30000 40000 50000
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0.0 0.6924 0.5193 0.3739 0.2423 0.1385 0.0865
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0.2 0.7415 0.5435 0.3886 0.2535 0.1535 0.0900
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0.4 0.7858 0.5837 0.4241 0.2823 0.1731 0.0981
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0.6 0.8392 0.6546 0.4764 0.3214 0.1973 0.1113
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0.8 0.9025 0.7296 0.5530 0.3848 0.2375 0.1367
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1.0 1.0000 0.8073 0.6335 0.4668 0.2992 0.1751
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1.2 1.0000 0.9000 0.7000 0.5300 0.4000 0.0200
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1.4 1.0000 0.9000 0.8000 0.6000 0.5000 0.0200
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</TABLE>
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</FG_TURBINE>
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