[fltsim.0]
title=AR9_ULM
sim=AR9_ULM
model=
panel=
sound=
texture=red_style
kb_checklists=
kb_reference=
atc_id=CU-U1517
atc_id_color=
ui_manufacturer=AEROPROYECTO
ui_type="AR9 ULM"
ui_variation="Red Style"
description="AR9 R1.0 FreeWare \nAEROPROYECTO 1999-2014 \nBy Edgar Guinart Lуpez\[email protected] \n\nThis model is a real project of ULM by Adolfo Rivera. For more detail chek out the document AR9 Real Project"

[General]
atc_type=ULM
atc_model=ULM
editable=0
performance=""


[WEIGHT_AND_BALANCE]
max_gross_weight = 860                         // (pounds)
empty_weight =  649                             // (pounds)  489 (EW) PLUS a pilot of 160 pounds

reference_datum_position     =  0, 0, 0         // (feet) distance from FlightSim Reference position: (1/4 chord, centerline, waterline)
empty_weight_CG_position     =  -0.75, 0, 0         // (feet) longitudinal, lateral, vertical distance from specified datum

max_number_of_stations =1

station_load.0 = "160.0, -1.40, 0.0, 0.0, Max 210 lbs"       //Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)

;Moments of Inertia
empty_weight_pitch_MOI   = 610
empty_weight_roll_MOI    =  450
empty_weight_yaw_MOI     = 690
empty_weight_coupled_MOI = 0.0


[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  = 0.0
rudder_trim_effectiveness   = 0.0
p_factor_on_yaw          = 0.3
torque_on_roll           = 0.3
gyro_precession_on_yaw   = 1.0
gyro_precession_on_pitch = 1.0

[exits]
number_of_exits = 2
exit_rate.0 = 0.8                               ;Percent per second
exit_rate.1 = 0.8                               ;Percent per second

[Flaps.0]
type= 0

[GeneralEngineData]
engine_type = 0                                 //0=Piston, 1=Jet, 2=None, 3=Helo-Turbine, 4=Rocket, 5=Turboprop
Engine.0 = 3.3, 0.0, 0.0                        //(feet) longitudinal, lateral, vertical distance from reference datum
fuel_flow_scalar= 1.9                           //Fuel flow scalar
min_throttle_limit = 0.0                        //Minimum percent throttle.  Generally negative for turbine reverser

[piston_engine]
power_scalar = 1.0                              //Piston power scalar  *** ROTAX 582
cylinder_displacement= 35.44                    //Cubic inches per cylinder  *** total 35.44
compression_ratio= 5.75                         //Compression ratio  *** Theoretical = 11.5:1 / Effective = 5.75:1
number_of_cylinders= 2                          //Number of cylinders
max_rated_rpm= 6200                             //Max rated RPM *** Theoretical = 6800 / Real est: 6200, but not use it!
max_rated_hp= 64                                //Max rated HP *** Real est: 64 hp at 6200 rpm
fuel_metering_type= 1                           //0=Fuel Injected, 1=Gravity Carburetor, 2=Aerobatic Carburetor
cooling_type= 1                                 //0=Cooling type Air, 1=Cooling type Liquid
normalized_starter_torque= 0.3                  //Starter torque factor
turbocharged= 0                                 //Is it turbocharged? 0=FALSE, 1=TRUE
max_design_mp= 0                                //Max design manifold pressure, (inHg)
min_design_mp= 0                                //Min design manifold pressure, (inHg)
critical_altitude= 0                            //Altitude to which the turbocharger will provide max design manifold pressure (feet)
emergency_boost_type= 0                         //0=None, 1=Water Injection, 2=Methanol/Water injection, 3=War Emergency Power
emergency_boost_mp_offset= 0                    //Additional manifold pressure supplied by emergency boost
emergency_boost_gain_offset= 0                  //Multiplier on manifold pressure due to emergency boost
fuel_air_auto_mixture= 0                        //Automixture available? 0=FALSE, 1=TRUE
auto_ignition= 0                                //Auto-Ignition available? 0=FALSE, 1=TRUE
max_rpm_mechanical_efficiency_scalar= 0.86       //Scalar on maximum RPM mechanical efficiency
idle_rpm_mechanical_efficiency_scalar= 1.1      //Scalar on idle RPM mechanical efficiency
max_rpm_friction_scalar= 1.0                    //Scalar on maximum RPM friction
idle_rpm_friction_scalar= 1.0                   //Scalar on idle RPM friction

[propeller]
thrust_scalar = 1.0                             //Propeller thrust scalar
propeller_type= 1                               //0=Constant Speed, 1=Fixed Pitch
propeller_diameter= 5.83                        //Propeller Diameter, (feet)
propeller_blades= 2                             //Number of propeller blades
propeller_moi= 3.50                             //Propeller moment of inertia
beta_max= 0                                     //Maximum blade pitch angle for constant speed prop, (degrees)
beta_min= 0                                     //Minimum blade pitch angle for constant speed prop, (degrees)
min_gov_rpm= 0                                  //Miminum governed RPM
prop_tc= 0.1                                    //Prop time-constant
gear_reduction_ratio= 3.0                       //Propeller gear reduction ratio  *** Real aprox 3.0, but not use it!
fixed_pitch_beta= 14.5                          //Fixed pitch angle of fixed pitch prop, (degrees)
low_speed_theory_limit= 50                      //Speed at which low speed theory becomes blended in (feet/second)
prop_sync_available= 0                          //Prop synchronization available? 0=FALSE, 1=TRUE
prop_deice_available= 0                         //Prop de-icing available? 0=FALSE, 1=TRUE
prop_feathering_available= 0                    //Prop feathering available?  0=FALSE, 1=TRUE
prop_auto_feathering_available= 0               //Prop auto-feathering available?  0=FALSE, 1=TRUE
min_rpm_for_feather= 0                          //Minimum RPM for prop feathering
beta_feather= 0.0                               //Feathering pitch angle (degrees)
power_absorbed_cf= 0                            //Coefficient of friction for power absorbed by propeller in feather
defeathering_accumulators_available= 0          //Defeathering accumulators available? 0=FALSE, 1=TRUE 
prop_reverse_available= 0                       //Prop reverse available?  0=FALSE, 1=TRUE
minimum_on_ground_beta= 0                       //Miminum pitch angle on ground, (degrees)
minimum_reverse_beta= 0                         //Minimum pitch angle in reverse, (degrees)


        //0  Class
        //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


[contact_points]
point.0 = 1,  -13.2,  0.0, -1.30, 1200, 0, 0.8,   28.0, 0.10, 2.5, 0.60, 0.0, 0.0, 0	//nose g
point.1 = 1,   0.45,  -3.0, -3.95, 1500, 1, 0.8,  0.000, 0.20, 2.5, 0.60, 0.0, 0.0, 2	//left g
point.2 = 1,   0.45,   3.0, -3.95, 1500, 2, 0.8,  0.000, 0.20, 2.5, 0.60, 0.0, 0.0, 3	//right g
//crash
point.3 = 2,   -1.6, -14.8,  2.00, 9999, 0, 0.0,  0.0,  0.0, 1.0, 1.0, 0.0, 0.0, 5	//left w
point.4 = 2,   -1.6,  14.8,  2.00, 9999, 0, 0.0,  0.0,  0.0, 1.0, 1.0, 0.0, 0.0, 6	//right w	
point.5=  2,   3.3,  -0.8, -1.65, 9999, 0, 0.0,  0.0,  0.0, 1.0, 1.0, 0.0, 0.0, 4		//l_nose f
point.6=  2,   3.3,   0.8, -1.65, 9999, 0, 0.0,  0.0,  0.0, 1.0, 1.0, 0.0, 0.0, 4		//r_nose f
point.7=  2,  -1.0,  -1.5, -1.65, 9999, 0, 0.0,  0.0,  0.0, 1.0, 1.0, 0.0, 0.0, 7		//left f
point.8=  2,  -1.0,   1.5, -1.65, 9999, 0, 0.0,  0.0,  0.0, 1.0, 1.0, 0.0, 0.0, 8		//right f
point.9=  2, -11.8,  -0.1,  -0.50, 9999, 0, 0.0,  0.0,  0.0, 1.0, 1.0, 0.0, 0.0, 9	//l_tail
point.10= 2, -11.8,   0.1,  -0.50, 9999, 0, 0.0,  0.0,  0.0, 1.0, 1.0, 0.0, 0.0, 9	//r_tail

static_pitch = 11.0
static_cg_height = 3.7

[brakes]
parking_brake = 1      		 //Parking brake available
toe_brakes_scale = 0.5  		 //Brake scalar
differential_braking_scale = 0.0             //Delta on the amount of brake when the rudder pedals deflected

[hydraulic_system]
normal_pressure = 0.0    //PSI

[Views]
eyepoint = -1.5, -0.69, 1.3

[LIGHTS]
//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing
light.0 = 4,  -1.1,   0.00,  1.50, fx_vclight,

[Radios]
// Radio Type = availiable, standby frequency, has glide slope
Audio.1       = 0
Com.1         = 1, 0
Nav.1         = 0, 0, 0
Adf.1         = 0
Transponder.1 = 0
Marker.1      = 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 =200, 1000
aileron  =200, 1000
rudder   =200, 1000

[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=0,0

[attitude_indicators]
//Type: 0=None, 1=Vacuum Gyro, 2=Electric Gyro
attitude_indicator.0 = 0 

[turn_indicators]
//Type: 0=None, 1=Electric Gyro, 2= Vacuum Gyro
turn_indicator.0=0,0

[EFFECTS]
wake=fx_wake
water=fx_spray
dirt=fx_tchdrt
concrete=fx_sparks
startup=fx_engstrt_cub
touchdown=fx_tchdwn_s, 1

[electrical]
max_battery_voltage = 0
generator_alternator_voltage = 13.8
max_generator_alternator_amps = 40.0

[fuel]
LeftMain  = 0.0, -3.0, 1.9, 3.75, 0.0       //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)
RightMain = 0.0,  3.0, 1.9, 3.75, 0.0       //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)(gallons)
fuel_type = 1                                //Fuel type: 1 = Avgas, 2 = JetA
number_of_tank_selectors = 1                    
electric_pump=1

[airplane_geometry]
wing_area               = 151.0                 //Square feet
wing_span               = 30.9                  //Feet
wing_root_chord         = 5.0                   //Feet
wing_dihedral           = 2.0                   //Degrees
wing_incidence          = 2.5                   //Degrees
wing_twist              = 0.0                   //Degrees
oswald_efficiency_factor= 0.8                   //Measure of lift effeciency of wing
wing_winglets_flag      = 0                     //Are winglets available?
wing_sweep              = 0.0                   //Degrees, wing leading edge
wing_pos_apex_lon       = 0.42                  //Feet, longitudinal distance from reference point, negative going aft
wing_pos_apex_vert      = 1.8                   //Feet, vertical distance from reference point, positive going up

htail_area              = 23.68                 //Square feet
htail_span              = 8.2                   //Feet
htail_pos_lon           = -10.5                 //Feet, longitudinal distance from reference point, negative going aft
htail_pos_vert          = 0.1                   //Feet, vertical distance from reference point, positive going up
htail_incidence         = -1.0                   //Degrees
htail_sweep             = 0.0                   //Degrees, horizontal tail leading edge

vtail_area              = 9.47                  //Square feet
vtail_span              = 2.95                  //Feet, tip to body
vtail_sweep             = 47.0                  //Degrees, vertical tail leading edge
vtail_pos_lon           = -10.2                 //Feet, longitudinal distance from reference point, negative going aft
vtail_pos_vert          = 1.6                   //Feet, vertical distance from reference point, positive going up

elevator_area           = 9.7                   //Square feet
aileron_area            = 15.21                 //Square feet
rudder_area             = 4.61                  //Square feet
elevator_up_limit       = 30.0                  //Degrees
elevator_down_limit     = 20.0                  //Degrees
aileron_up_limit        = 20.0                  //Degrees
aileron_down_limit      = 20.0                  //Degrees
rudder_limit            = 28.0                  //Degrees
elevator_trim_limit     = 10.0                  //Degrees
spoiler_limit           = 0.0                   //Degrees
spoilerons_available    = 0                     //Spoilerons Available?
aileron_to_spoileron_gain = 0                   //Aileron to spoileron gain
min_ailerons_for_spoilerons = 0                 //Degrees
min_flaps_for_spoilerons = 0                    //Minimum flap handle position when spoilerons activate

[Reference Speeds]
flaps_up_stall_speed    = 33.0                  //Knots True (KTAS)
full_flaps_stall_speed  = 33.0                  //Knots True (KTAS)
cruise_speed            = 63.0                  //Knots True (KTAS)
max_indicated_speed     = 87                    //Red line (KIAS)

[autopilot]
autopilot_available= 0
flight_director_available= 0

[forcefeedback]
ground_bumps_magnitude1=2600            ; 0 - 10000
ground_bumps_angle1=8900                ; 0 - 35999 degrees
ground_bumps_intercept1=5.0
ground_bumps_slope1=0.6
ground_bumps_magnitude2=1200            ; 0 - 10000
ground_bumps_angle2=9100                ; 0 - 35999 degrees
ground_bumps_intercept2=0.085
ground_bumps_slope2=0.65
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=3500000                 ; in microseconds

[stall_warning]
type=1