<?xml version="1.0"?> <!-- PT6A-68 turboprop engine model for the SimTurbine turbine model --> <FG_SIMTURBINE NAME="PT6A-68"> <!-- MILTHRUST max static thrust at S.L. (installed), lbf MAXTHRUST max static thrust with afterburning at S.L. (installed), lbf BYPASSRATIO bypass ratio TSFC thrust-specific fuel consumption (lbm/hr/lbf) ATSFC augmented TSFC (lbm/hr/lbf) IDLEN1 idle percent rpm of fan spool IDLEN2 idle percent rpm of inner spool MAXN1 N1 at 100% throttle MAXN2 N2 at 100% throttle AUGMENTED = 1 if augmentation installed, else = 0 AUGMETHOD = 0 if using property /engine[n]/augmentation = 1 if using last 1% of throttle movement INJECTED = 1 if water injection installed TABLE(0) idle thrust vs. altitude and mach TABLE(1) maximum un-augmented thrust vs. altitude and mach TABLE(2) augmented thrust multiplier vs. altitude and mach TABLE(3) water-injection multiplier vs. altitude and mach --> <!-- 1100 horsepower X 2.24 lb/hp --> MILTHRUST 2464 MAXTHRUST 2464 BYPASSRATIO 0 TSFC 0.55 ATSFC 0.00 IDLEN1 0.0 IDLEN2 65.0 MAXN1 0.0 MAXN2 100.0 AUGMENTED 0 AUGMETHOD 0 INJECTED 0 <TABLE NAME="IdleThrust" TYPE="TABLE"> Idle_power_thrust_factor 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_factor 6 6 velocities/mach-norm position/h-sl-ft none 0 10000 20000 30000 40000 50000 0.0 1.0000 0.7400 0.5340 0.3720 0.2410 0.1490 0.2 0.7340 0.6970 0.5060 0.3550 0.2310 0.1430 0.4 0.6210 0.5920 0.4060 0.3570 0.2330 0.1450 0.6 0.3510 0.2710 0.2020 0.1780 0.1020 0.0640 0.8 0.0200 0.0200 0.0200 0.0200 0.0200 0.0200 1.0 0.0 0.0 0.0 0.0 0.0 0.0 </TABLE> </FG_SIMTURBINE>