[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