[fltsim.0] title=ME109_G sim=ME109_G model= panel= sound= texture= ui_manufacturer=MESSERSCHMITT ui_type=ME109_G ui_variation=Gustav kb_checklists= description=Notes:The German Messerschmitt based his design on the experiance he had gained with the Bf 108. It was an excellent lightweight plane, which was superior to the modern fighter planes used by some nations at that time. So Messerschmitt optimized the fuselage, reduced the weight and fitted this design with the most powerful engine available at that time. [fltsim.1] title=ME109_GPaint1 sim=ME109_G model= panel= sound= ui_manufacturer=MESSERSCHMITT ui_type= ME109_G_ ANR ui_variation=Gustav ANR texture=1 kb_checklists= description=Notes:The German Messerschmitt based his design on the experiance he had gained with the Bf 108. It was an excellent lightweight plane, which was superior to the modern fighter planes used by some nations at that time. So Messerschmitt optimized the fuselage, reduced the weight and fitted this design with the most powerful engine available at that time. atc_heavy=0 atc_id=1769 atc_airline=one 4 atc_flight_number=xgust [WEIGHT_AND_BALANCE] performance=Length:8.94m\nWing span:9.92m\nWeight:MTOW 3200 kg\n Empty 2709 kg\nPower:1xDaimler Benz 605A1,475Hp\nDetails:\nDesigners:ItaloD'Attomo and Giovanni Quai\nDate:November 2005\n\n reference_datum_position=0.000000,0.000000,0.000000 empty_weight_CG_position=0.000000,0.000000,0.000000 empty_weight=6285.000000 empty_weight_roll_MOI=14097.000000 empty_weight_pitch_MOI=10138.000000 empty_weight_yaw_MOI=20372.000000 empty_weight_coupled_MOI=0.000000 max_gross_weight=7054.000000 [flight_tuning] cruise_lift_scalar = 1 parasite_drag_scalar = 0.6 induced_drag_scalar = 1.4 elevator_effectiveness = 1 aileron_effectiveness = 1.5 rudder_effectiveness = 1 pitch_stability = 1 roll_stability = 1 yaw_stability = 1 elevator_trim_effectiveness = 1.3 aileron_trim_effectiveness = 1 rudder_trim_effectiveness = 1 [piston_engine] power_scalar = 1 cylinder_displacement = 148.888888888889 compression_ratio = 8 number_of_cylinders = 12 max_rated_rpm = 3000 max_rated_hp = 1775 fuel_metering_type = 1 cooling_type = 1 normalized_starter_torque = 0.07 turbocharged = 1 max_design_mp = 54 min_design_mp = 9 critical_altitude = 5100 emergency_boost_type = 0 emergency_boost_mp_offset = 0 emergency_boost_gain_offset = 0 fuel_air_auto_mixture = 0 auto_ignition = 0 max_rpm_mechanical_efficiency_scalar = 1 idle_rpm_mechanical_efficiency_scalar = 1 max_rpm_friction_scalar = 1 idle_rpm_friction_scalar = 1 [propeller] thrust_scalar = 1 propeller_type = 0 propeller_diameter = 9 propeller_blades = 3 propeller_moi = 14.1 beta_max = 65 beta_min = 15 min_gov_rpm = 337.5 prop_tc = 0.01 gear_reduction_ratio = 1 fixed_pitch_beta = 30 low_speed_theory_limit = 80 prop_sync_available = 0 prop_deice_available = 0 prop_feathering_available = 0 prop_auto_feathering_available = 0 min_rpm_for_feather = 700 beta_feather = 88.5 power_absorbed_cf = 0.9 defeathering_accumulators_available = 0 prop_reverse_available = 0 minimum_on_ground_beta = 1 minimum_reverse_beta = -14 rotation = 1 [contact_points] max_number_of_points = 9 point.0 = 1, -16.2, 0, -2.1, 1600, 0, 0.531197, 41.64, 0.551117, 2.5, 0.686607, 5, 5, 0, 0, 0 point.1 = 1, 4.3, -4, -6.1, 1600, 1, 0.531197, 0, 0.714684, 2.5, 0.274063, 4.1, 4.1, 2, 0, 0 point.2 = 1, 4.3, 4, -6.1, 1600, 2, 0.531197, 0, 0.714684, 2.5, 0.274063, 8.2, 8.2, 3, 0, 0 point.3 = 2, -1, -21.6, 0.2, 1600, 0, 0, 0, 0, 0, 0, 0, 0, 5 point.4 = 2, -1, 21.6, 0.2, 1600, 0, 0, 0, 0, 0, 0, 0, 0, 6 point.5 = 2, -19.4, 0, 0.9, 1600, 0, 0, 0, 0, 0, 0, 0, 0, 9 point.6 = 2, 0, 0, -2.2, 1600, 0, 0, 0, 0, 0, 0, 0, 0, 4 point.7 = 2, 10, 0, 0.2, 1600, 0, 0, 0, 0, 0, 0, 0, 0, 4 point.8 = 2, 9.8, 0, -4, 1600, 0, 0, 0, 0, 0, 0, 0, 0, 4 static_pitch= 12 static_cg_height= 4.90927 gear_system_type=1 [Views] eyepoint= -0.2, 0, 3.35 [flaps.0] //Trailing Edge Flaps type = 1 span-outboard = 0.5 extending-time = 5 flaps-position.0 = 0 flaps-position.1 =10 flaps-position.2 = 16 flaps-position.3 = 25 flaps-position.4 = 35 damaging-speed = 145 blowout-speed = 125 [Flaps.1] type=2 span-outboard=0.5 extending-time=5. system_type=0 flaps-position.0=0. flaps-position.1=100 [electrical] max_battery_voltage = 24 generator_alternator_voltage = 28 max_generator_alternator_amps = 160 electric_always_available = 1 flap_motor = 0, 5, 17 gear_motor = 0, 5, 17 autopilot = 0, 5, 17 avionics_bus = 0, 10, 17 avionics = 1, 5, 17 pitot_heat = 0, 2, 17 additional_system = 0, 20, 17 marker_beacon = 1, 2, 17 gear_warning = 0, 2, 17 fuel_pump = 0, 5, 17 starter1 = 0, 20, 17 starter2 = 0, 20, 17 starter3 = 0, 20, 17 starter4 = 0, 20, 17 light_nav = 0, 5, 17 light_beacon = 0, 5, 17 light_landing = 0, 5, 17 light_taxi = 0, 5, 17 light_strobe = 0, 5, 17 light_panel = 0, 5, 17 prop_sync = 0, 15, 17 auto_feather = 0, 15, 17 auto_brakes = 0, 15, 17 standby_vacuum = 0, 15, 17 hydraulic_pump = 0, 2, 17 fuel_transfer_pump = 0, 5, 17 propeller_deice = 0, 5, 17 light_recognition = 0, 5, 17 light_wing = 0, 5, 17 light_logo = 0, 5, 17 [LIGHTS] //Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit light.0=3, 5.70, -16.40, 0.16, fx_navred light.1=3, 5.70, 16.40, 0.16, fx_navgre panel = 0, 0.35, -0.8, fx_vclight [LSO] LSOAdjustSpeed = 1.2 [exits] number_of_exits = 1 exit_rate.0 = 0.4 [General] performance=Max Weight 7054 lbs\n Power: 1475 hp\nMax speed @ SL: 326 mph (525Kmh)\n Max speed@ 7000 mt: 403 mph(650 kmh) \n [fuel] LeftMain=0.000000,-2.500000,0.000000,55.500000,0.000000 RightMain=0.000000,2.500000,0.000000,55.500000,0.000000 fuel_type=1.000000 number_of_tank_selectors=1 electric_pump=1 [airplane_geometry] wing_area=254.000000 wing_span=42.000000 wing_root_chord=7.500000 wing_dihedral=5.597534 wing_incidence=0.000000 wing_twist=0.000000 oswald_efficiency_factor=0.891323 wing_winglets_flag=0 wing_sweep=0.000000 wing_pos_apex_lon=1.510119 wing_pos_apex_vert=0.000000 htail_area=34.000000 htail_span=13.000000 htail_pos_lon=-17.916667 htail_pos_vert=0.000000 htail_incidence=0.000000 htail_sweep=0.000000 vtail_area=19.000000 vtail_span=4.969909 vtail_sweep=0.000000 vtail_pos_lon=-19.500000 vtail_pos_vert=7.250000 elevator_area=26.600000 aileron_area=18.900000 rudder_area=14.900000 elevator_up_limit=30.000000 elevator_down_limit=20.000000 aileron_up_limit=15.000000 aileron_down_limit=15.000000 rudder_limit=30.000000 elevator_trim_limit=18.000000 spoiler_limit=0.000000 spoilerons_available=0 aileron_to_spoileron_gain=0.000000 min_ailerons_for_spoilerons=0.000000 min_flaps_for_spoilerons=0.000000 [brakes] toe_brakes_scale=0.885 parking_brake=1 [gear_warning_system] gear_warning_available=0 pct_throttle_limit=0.099976 flap_limit_power=33.750000 flap_limit_idle=16.875000 [GeneralEngineData] engine_type=0 Engine.0=9.750000,0.000000,0.000000 fuel_flow_scalar=1.000000 min_throttle_limit=0.000000 [Reference Speeds] flaps_up_stall_speed=73 full_flaps_stall_speed=58 cruise_speed=250 max_indicated_speed=503 [keyboard_response] elevator=350.000000,500.000000 aileron=450.000000,1000.000000 rudder=200.000000,1000.000000 [autopilot] autopilot_available=1 flight_director_available=0 default_vertical_speed=700.000000 autothrottle_available=0 pitch_takeoff_ga=8.000000 max_pitch=10.000000 max_pitch_acceleration=1.000000 max_pitch_velocity_lo_alt=2.000000 max_pitch_velocity_hi_alt=1.500000 max_pitch_velocity_lo_alt_breakpoint=20000.000000 max_pitch_velocity_hi_alt_breakpoint=28000.000000 max_bank=25.000000 max_bank_acceleration=1.800000 max_bank_velocity=3.000000 max_throttle_rate=0.100000 nav_proportional_control=9.000000 nav_integrator_control=0.250000 nav_derivative_control=0.000000 nav_integrator_boundary=2.500000 nav_derivative_boundary=0.000000 gs_proportional_control=9.520000 gs_integrator_control=0.260000 gs_derivative_control=0.000000 gs_integrator_boundary=0.700000 gs_derivative_boundary=0.000000 yaw_damper_gain=0.000000 [hydraulic_system] electric_pumps=0 engine_map=1,0,0,0 normal_pressure=6.930556 [stall_warning] type=1 [attitude_indicators] attitude_indicator.0=1 [turn_indicators] turn_indicator.0=1,0 [direction_indicators] direction_indicator.0=1,0