<?xml version="1.0"?> <turbine_engine name="APS3200"> <milthrust> 2.6 </milthrust> <bypassratio> 0.000 </bypassratio> <tsfc> 0.820 </tsfc> <bleed> 0.96</bleed> <!-- 16 / 400 KW exhaust energy --> <!-- self sustaining speed is 55.0 --> <ignitionn1> 5.0</ignitionn1> <ignitionn2> 26</ignitionn2> <!-- hack to make work --> <n1spinup> 3.0</n1spinup> <n2spinup> 8.666</n2spinup> <!-- hack to make work --> <n1startrate> 1.8222</n1startrate> <n2startrate> 1.8222</n2startrate> <idlen1> 99.9 </idlen1> <idlen2> 99.9 </idlen2> <n1spindown> 20</n1spindown> <n2spindown> 20</n2spindown> <disable-windmill> 1</disable-windmill> <maxn1> 100.0 </maxn1> <maxn2> 100.0 </maxn2> <augmented> 0 </augmented> <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 90000 0.0 0.0430 0.0488 0.0528 0.0694 0.0899 0.1183 0.1467 0 0.2 0.0500 0.0501 0.0335 0.0544 0.0797 0.1049 0.1342 0 0.4 0.0040 0.0047 0.0020 0.0272 0.0595 0.0891 0.1203 0 0.6 -0.0804 -0.0804 -0.0560 -0.0237 0.0276 0.0718 0.1073 0 0.8 -0.2129 -0.2129 -0.1498 -0.1025 0.0474 0.0868 0.0900 0 1.0 -0.2839 -0.2839 -0.1104 -0.0469 -0.0270 0.0552 0.0800 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 90000 0.0 1.2600 1.0000 0.7400 0.5340 0.3720 0.2410 0.1490 0.0580 0 0.2 1.1692 0.9326 0.6959 0.5052 0.3545 0.2306 0.1428 0.0399 0 0.4 1.1465 0.9182 0.6899 0.5044 0.3559 0.2323 0.1446 0.0429 0 0.6 1.1755 0.9466 0.7177 0.5295 0.3763 0.2469 0.1533 0.0468 0 0.8 1.2503 1.0137 0.7772 0.5784 0.4144 0.2733 0.1690 0.0527 0 1.0 1.3585 1.1114 0.8643 0.6460 0.4713 0.3126 0.1935 0.0625 0 1.2 1.4713 1.2186 0.9660 0.7371 0.5400 0.3606 0.2229 0.0733 0 1.4 1.5769 1.3256 1.0743 0.8359 0.6212 0.4194 0.2602 0.0890 0 </tableData> </table> </function> </turbine_engine>