[fltsim.0] title=SS_O'Higgins sim=Scorpene model= panel= sound= texture= kb_checklists=Cessna208B_Check kb_reference=Cessna208B_ref atc_id_color=0xff000000 atc_id= atc_airline= atc_flight_number= atc_parking_types=GATE,RAMP ui_manufacturer=Juan Design ui_type=Scorpene ui_variation=O'Higgins description=Unidad recientemente adquirida por la Armada de Chile, especial para operar en misiones oceánicas, antisubmarinas y de lucha antisuperficie. Creado por Juan Guajardo S. Septiembre 2008. Model creado en Gmax. atc_parking_codes=HMS [pitot_static] vertical_speed_time_constant=1 //Increasing this value will cause a more instantaneous reaction in the VSI [WEIGHT_AND_BALANCE] max_gross_weight=70000 // (pounds) empty_weight=70000 // (pounds) reference_datum_position=61.0, 0, 0 // (feet) distance from FlightSim Reference position: (1/4 chord, centerline, waterline) empty_weight_CG_position=-120.5, 0, 0 // (feet) longitudinal, lateral, vertical distance from specified datum max_number_of_stations=50 ;Moments of Inertia empty_weight_roll_MOI=13352310 empty_weight_pitch_MOI=24223159 empty_weight_yaw_MOI=39531785 empty_weight_coupled_MOI=0 [fuel] LeftMain=-85.0, -28.0, -4.0, 12546.0, 0.0 //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons) RightMain=-85.0, 28.0, -4.0, 12546.0, 0.0 //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons) LeftAux=-112.0, -36.5, -3.0, 4482.0, 0.0 //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons) RightAux=-112.0, 36.5, -3.0, 4482.0, 0.0 //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons) LeftTip=-130.0, -73.0, 0.0, 1322.0, 0.0 //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons) RightTip=-130.0, 73.0, 0.0, 1322.0, 0.0 //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons) Center1=-83.5, 0.0, -7.0, 17164.0, 0.0 //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons) Center2=-193.5, 0.0, 6.0, 3300.0, 0.0 //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons) fuel_type=2 //Fuel type: 1 = Avgas, 2 = JetA number_of_tank_selectors=1 electric_pump=0 [airplane_geometry] wing_area=5825.0 //Square feet wing_span=211.4 //Feet wing_root_chord=48.8 //Feet wing_dihedral=7.0 //Degrees wing_incidence=2.0 //Degrees wing_twist=-1.0 //Degrees oswald_efficiency_factor=0.68 //Measure of lift effeciency of wing wing_winglets_flag=1 //Are winglets available? wing_sweep=37.5 //Degrees, wing leading edge wing_pos_apex_lon=-58.2 //Feet, longitudinal distance from reference point, negative going aft wing_pos_apex_vert=0 //Feet, vertical distance from reference point, positive going up htail_area=1470 //Square feet htail_span=72.8 //Feet htail_pos_lon=-210.0 //Feet, longitudinal distance from reference point, negative going aft htail_pos_vert=0.0 //Feet, vertical distance from reference point, positive going up htail_incidence=0.0 //Degrees htail_sweep=37.5 //Degrees, horizontal tail leading edge vtail_area=1060 //Square feet vtail_span=37.1 //Feet, tip to body vtail_sweep=45.0 //Degrees, vertical tail leading edge vtail_pos_lon=-198.5 //Feet, longitudinal distance from reference point, negative going aft vtail_pos_vert=26.1 //Feet, vertical distance from reference point, positive going up elevator_area=327 //Square feet aileron_area=225 //Square feet rudder_area=230 //Square feet elevator_up_limit=25 //Degrees elevator_down_limit=15 //Degrees aileron_up_limit=25 //Degrees aileron_down_limit=15 //Degrees rudder_limit=31.5 //Degrees elevator_trim_limit=20 //Degrees spoiler_limit=45 //Degrees spoilerons_available=1 //Spoilerons Available? aileron_to_spoileron_gain=3 //Aileron to spoileron gain min_ailerons_for_spoilerons=10 //Degrees min_flaps_for_spoilerons=0 //Minimum flap handle position when spoilerons activate [Reference Speeds] flaps_up_stall_speed=140.0 //Knots True (KTAS) full_flaps_stall_speed=112.0 //Knots True (KTAS) cruise_speed=505.0 //Knots True (KTAS) max_mach=0.92 max_indicated_speed=365.0 //Red line (KIAS) [flaps.0] type=1 // 1 - tail, 2 - lead span-outboard=0.8 // 0.0 .. 1.0 extending-time=25 // seconds flaps-position.0=0 // degrees flaps-position.1=1 // degrees flaps-position.2=5 // degrees flaps-position.3=10 // degrees flaps-position.4=20 // degrees flaps-position.5=25 // degrees flaps-position.6=30 // degrees damaging-speed=200 // KIAS blowout-speed=250 // KIAS lift_scalar=0.7 drag_scalar=0.9 pitch_scalar=0.9 system_type=1 //Hydraulic [flaps.1] type=2 // 1 - tail, 2 - lead span-outboard=0.8 // 0.0 .. 1.0 extending-time=2 // seconds flaps-position.0=0 // degrees flaps-position.1=1.0 // degrees damaging-speed=250 // KIAS blowout-speed=300 // KIAS lift_scalar=0.3 drag_scalar=0.1 pitch_scalar=0.1 system_type=1 //Hydraulic [flight_tuning] cruise_lift_scalar=1.0 parasite_drag_scalar=1.0 induced_drag_scalar=1.0 elevator_effectiveness=1.0 aileron_effectiveness=1.0 rudder_effectiveness=1.0 pitch_stability=1.0 roll_stability=1.0 yaw_stability=1.0 elevator_trim_effectiveness=1.0 aileron_trim_effectiveness=1.0 rudder_trim_effectiveness=1.0 [GeneralEngineData] engine_type=1 //0=Piston, 1=Jet, 2=None, 3=Helo-Turbine, 4=Rocket, 5=Turboprop Engine.0=-107.5, -69.5, -6.9 //(feet) longitudinal, lateral, vertical distance from reference datum Engine.1=-107.5, 69.5, -6.9 //(feet) longitudinal, lateral, vertical distance from reference datum fuel_flow_scalar=1.0 //Scalar for fuel flow efficiency min_throttle_limit=-0.25; //Minimum percent throttle. Generally negative for turbine reverser [TurbineEngineData] fuel_flow_gain=0.002 //Gain on fuel flow inlet_area=60.0 //Square Feet, engine nacelle inlet area rated_N2_rpm=29920 //RPM, second stage compressor rated value static_thrust=56750 //Lbs, max rated static thrust at Sea Level afterburner_available=0 //Afterburner available? reverser_available=1 //Thrust reverser available? [jet_engine] thrust_scalar=1.0 [autopilot] autopilot_available=1 flight_director_available=1 default_vertical_speed=1800.0 autothrottle_available=1 autothrottle_arming_required=1 autothrottle_max_rpm=90 autothrottle_takeoff_ga=1 pitch_takeoff_ga=8; max_pitch=10.0 max_pitch_acceleration=1.0 max_pitch_velocity_lo_alt=2.0 max_pitch_velocity_hi_alt=1.5 max_pitch_velocity_lo_alt_breakpoint=20000.0 max_pitch_velocity_hi_alt_breakpoint=28000.0 max_bank=25.0 max_bank_acceleration=1.8 max_bank_velocity=3.00 max_throttle_rate=0.10 nav_proportional_control=16.00 nav_integrator_control=0.17 nav_derivative_control=0.00 nav_integrator_boundary=2.50 nav_derivative_boundary=0.00 gs_proportional_control=18.0 gs_integrator_control=0.33 gs_derivative_control=0.00 gs_integrator_boundary=0.70 gs_derivative_boundary=0.00 yaw_damper_gain=1.0 [contact_points] ;/0 Class <0=none,1=wheel, 2=scrape, 3=float> ;/1 Longitudinal Position (feet) ;/2 Lateral Position (feet) ;/3 Vertical Position (feet) ;/4 Impact Damage Threshold (Feet Per Minute) ;/5 Brake Map (0=None, 1=Left, 2=Right) ;/6 Wheel Radius (feet) ;/7 Steer Angle (degrees) ;/8 Static Compression (feet) (0 if rigid) ;/9 Max/Static Compression Ratio ;/10 Damping Ratio (0=Undamped, 1=Critically Damped) ;/11 Extension Time (seconds) ;/12 Retraction Time (seconds) ;/13 Sound Type ;/14 Airspeed limit for retraction (KIAS) ;/15 Airspeed that gear gets damage at (KIAS) point.0=1, 10.15, 0.00, -3.600, 5000, 0, 1.40, 10.0, 0.3, 2.5, 0.8, 1.0, 1.0, 0, 175.0, 175.0 point.1=1, -86.40, -6.250, -3.600, 5000, 1, 1.50, 0.0, 0.4, 2.5, 0.8, 0.0, 0.0, 1, 175.0, 175.0 point.2=1, -86.40, 6.250, -3.600, 5600, 2, 1.50, 0.0, 0.4, 2.5, 0.8, 0.0, 0.0, 2, 175.0, 175.0 point.3=4, 0.0, -2.0, -3.4, 5000.0, 0, 2.0, 0.0, 0.5, 2.5, 0.900, 0.0, 0.0, 0, 220, 250 point.4=4, 0.0, 2.0, -3.4, 5000.0, 0, 2.0, 0.0, 0.5, 2.5, 0.900, 0.0, 0.0, 0, 220, 250 point.5=4, -152.0, -15.0, -3.2, 5000.0, 1, 2.0, 10.0, 1.0, 2.0, 0.900, 0.0, 0.0, 2, 220, 250 point.6=4, -152.0, 15.0, -3.2, 5000.0, 2, 2.0, 10.0, 1.0, 2.0, 0.900, 0.0, 0.0, 3, 220, 250 static_pitch=-0.0 static_cg_height=3.5 gear_system_type=1 //Hydraulic [gear_warning_system] gear_warning_available=1 //Normal pct_throttle_limit=0.1 //Percent throttle that activates warning flap_limit_idle=5.0 //Flap angle that activates warning at idle flap_limit_power=25.5 //Flap angle that activates warning at above idle [brakes] parking_brake=1 //Parking brake available toe_brakes_scale=1.24 //Brake scalar [hydraulic_system] normal_pressure=3000.0 //PSI electric_pumps=0 //no electric pumps engine_map=1,1,1,1 //pumps on Eng1,2,3,4 [electrical] ;BusType, MaxAmpLoad, MinVoltage BusTypes:0=MainBus,1=AvionicsBus,2=BatteryBus,3=HotBatteryBus,4-7=Generator/AlternatorBus(1-4) autopilot=0, 5 , 17.0 avionics_bus=0, 5 , 17.0 avionics=1, 5 , 17.0 gear_warning=0, 2 , 17.0 fuel_pump=0, 5 , 17.0 light_nav=0, 5 , 17.0 light_beacon=0, 5 , 17.0 light_landing=0, 5 , 17.0 light_taxi=0, 5 , 17.0 light_strobe=0, 5 , 17.0 light_panel=0, 5 , 17.0 [Radios] ;/ Radio Type = availiable, standby frequency, has glide slope Audio.1=1 Com.1=1, 1 Com.2=1, 1 Nav.1=1, 1, 1 Nav.2=1, 1, 0 Adf.1=1 Transponder.1=1 Marker.1=1 [SMOKESYSTEM] smoke.0=0, 55.0, 0.0, fx_Smoke_lf.fx, smoke.1=0, -545.0, 4.0, fx_sprayll.fx, smoke.2=0, -545.0, -4.0, fx_sprayll.fx, smoke.3=0, -520.0, 16.0, fx_sprayll.fx, smoke.4=0, -520.0, -16.0, fx_sprayll.fx, smoke.5=0, -225.0, 0.0, fx_Smoke_lf.fx, [Views] eyepoint=200.00, -6.0,82.0 //Upper Deck //eyepoint=185.00, 42.0,75.0 // right wing ; Longitude, Latitude and Vertical position from Reference Point, (FEET) [direction_indicators] ;/1 Type: 0=None, 1=Vacuum Gyro, 2=Electric Gyro, 3=Electro-Mag Slaved Compass, 4=Slaved to another ;/2 Indicator number of slaving indicator if Type = 4 direction_indicator.0=3,0 [attitude_indicators] ;/Type: 0=None, 1=Vacuum Gyro, 2=Electric Gyro attitude_indicator.0=2 attitude_indicator.1=1 [turn_indicators] ;/Type: 0=None, 1=Electric Gyro, 2= Vacuum Gyro turn_indicator.0=0,0 [keyboard_response] ;/Breakpoint speeds (knots) on the keyboard increments of control surfaces. ;/Speed at which the incremenet is reduced to 1/2 and 1/8 respectively. elevator=150, 250 aileron=150, 250 rudder=150, 250 [EFFECTS] wake=fx_wake_l water=fx_spray_qm2 dirt=fx_tchdrt concrete=fx_sparks touchdown=fx_tchdwn, 1 [exits] number_of_exits=2 exit_rate.0=0.4 ;Percent per second exit_rate.1=0.4 ;Percent per second [folding_wings] wing_fold_system_type=4 ;0=None fold_rates=0.2,0.2 ;Percent per second [forcefeedback] gear_bump_nose_magnitude=3000 ; 0 - 10000 gear_bump_nose_direction=18000 ; 0 - 35999 degrees gear_bump_nose_duration=250000 ; in microseconds gear_bump_left_magnitude=2700 ; 0 - 10000 gear_bump_left_direction=35500 ; 0 - 35999 degrees gear_bump_left_duration=250000 ; in microseconds gear_bump_right_magnitude=2700 ; 0 - 10000 gear_bump_right_direction=00500 ; 0 - 35999 degrees gear_bump_right_duration=250000 ; in microseconds ground_bumps_magnitude1=1300 ; 0 - 10000 ground_bumps_angle1=08900 ; 0 - 35999 degrees ground_bumps_intercept1=3.0 ground_bumps_slope1=0.20 ground_bumps_magnitude2=200 ; 0 - 10000 ground_bumps_angle2=09100 ; 0 - 35999 degrees ground_bumps_intercept2=1.075 ground_bumps_slope2=0.035 crash_magnitude1=10000 ; 0 - 10000 crash_direction1=01000 ; 0 - 35999 degrees crash_magnitude2=10000 ; 0 - 10000 crash_direction2=9000 ; 0 - 35999 degrees crash_period2=75000 ; in microseconds crash_duration2=2500000 ; in microseconds [stall_warning] type=2 [General] performance= \n \n \n \n \n \n
