[fltsim.0]
title=Rotorway Exec 162f/mba 2
sim=Rotorway_Exec_162f
model=
panel=
sound=
texture=
kb_checklists=rotorway_162piston_check
kb_reference=rotorway_ref
prop_anim_ratio=-.80
atc_id_color=0xc6eff7ff
atc_id=459 MT
atc_model=
ui_manufacturer=RotorWay International
ui_type=Pilot PassengerDoors
ui_variation=Red and Black
description="A REVOLUTION IN TECHNOLOGY Combining a technological breakthrough in powerplant design with refinements to a highly successful, award winning airframe, the new Exec 162F has elevated a tradition into a revolution in helicopter performance."

[General]
atc_type=Helicopter
performance=Cruise Speed \t\n95 kts            110 mph          213 km\/h\n\nEngine\nRI 162F, 162 cu. in. (2659 cc) \n\nMaximum Range\n180 mi 2 hrs.   \t        \n\nService Ceiling\n10,000 ft m\n\nHovering Ceiling\n5,000            7,000 m\n\nFuel Capacity\n17 U.S. Gallons (64 liters). gal       \n\nEmpty Weight\n975 lbs. (442 kg)\n\nMaximum Gross Weight\n1500 lbs. (680 kg)\n\nMaximum Gross Weight (External Loading)\n0 lb          0 kg\n\nLength\t\n22 ft. \t         (6.7 meters) m\n\nRotor Span\n25.0 ft\t         7.6 m\n\nHeight\n96 in. \t         (2.4 meters) m\n\nSeating \t\n2 \n\nUseful Load\t\n525 lb\t          238 kg\n
editable=0

[WEIGHT_AND_BALANCE]
max_gross_weight = 1500                          // (pounds)
empty_weight = 975                            // (pounds)

reference_datum_position     =  8.33,  0.0, 0.0   // (feet) distance from FlightSim Reference position: (1/4 chord, centerline, waterline)
empty_weight_CG_position     = -9.09,  0.0, 0.0   // (feet) longitudinal, lateral, vertical distance from specified datum

max_number_of_stations = 50

station_load.0 = "160, -6.0,  -0.89, 0.0, Pilot"          // Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.1 = "160, -6.0, 0.89, 0.0, Passenger"      // Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.2 = "25, -11.0, 0.0, 0.0, Ballast"      // Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)


;Moments of Inertia
empty_weight_pitch_MOI   =  6000
empty_weight_roll_MOI    =  4000
empty_weight_yaw_MOI     = 10000
empty_weight_coupled_MOI =     0

[electrical]
                ;BusType, MaxAmpLoad, MinVoltage       BusTypes:0=MainBus,1=AvionicsBus,2=BatteryBus,3=HotBatteryBus,4-7=Generator/AlternatorBus(1-4)
flap_motor         = 0, 5 , 17.0
gear_motor         = 0, 5 , 17.0
autopilot          = 0, 5 , 17.0
avionics_bus       = 0, 5 , 17.0
avionics           = 1, 5 , 17.0
pitot_heat         = 0, 2 , 17.0
additional_system  = 0, 2 , 17.0
marker_beacon      = 1, 2 , 17.0
gear_warning       = 0, 2 , 17.0
fuel_pump          = 0, 5 , 17.0
starter1           = 0, 20, 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



        //0  Class                        <0=none,1=wheel, 2=scrape, 3=skid>
        //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)

 [contact_points]
point.0=3,   -2.74,  -3.13, -4.23, 1600, 0, 0.00, 0.0, 0.28, 2.5, 0.82, 0.0, 0.0, 7, 0.0, 0.0
point.1=3,   -2.74,   3.13, -4.23, 1600, 0, 0.00, 0.0, 0.28, 2.5, 0.82, 0.0, 0.0, 7, 0.0, 0.0
point.2=3,  -15.00,  -3.13, -4.16, 1600, 0, 0.00, 0.0, 0.28, 2.5, 0.82, 0.0, 0.0, 7, 0.0, 0.0
point.3=3,  -15.00,   3.13, -4.16, 1600, 0, 0.00, 0.0, 0.28, 2.5, 0.82, 0.0, 0.0, 7, 0.0, 0.0
point.4=2,   -8.50, -11.80,  5.30,  100, 0, 0, 0.0, 0.00, 0.0, 0.00, 0.0, 0.0, 5, 0.0, 0.0
point.5=2,   -8.50,  11.80,  5.30,  100, 0, 0, 0.0, 0.00, 0.0, 0.00, 0.0, 0.0, 6, 0.0, 0.0
point.6=2,    3.00,   0.00,  5.30,  100, 0, 0, 0.0, 0.00, 0.0, 0.00, 0.0, 0.0, 4, 0.0, 0.0
point.7=2,  -23.00,   0.00, -0.60,  300, 0, 0, 0.0, 0.00, 0.0, 0.00, 0.0, 0.0, 9, 0.0, 0.0

static_pitch = 1.4
static_cg_height = 3.58

[brakes]
parking_brake = 0       //Parking brake available
toe_brakes_scale = 0.0  //Brake scalar

[hydraulic_system]
normal_pressure = 0.0    //PSI

[Views]
eyepoint=-6.85, -0.8, 1.035 //(feet) longitudinal, lateral, vertical
//eyepoint=-6.50, -0.8, 1.40 //Track IR settings

[LIGHTS]
//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing
light.0 = 3, -5.35, -1.93, -1.90,  fx_navred_rway ,
light.1 = 3, -5.35,  1.93, -1.90,  fx_navgre_rway ,
light.2 = 3, -23.80,  0.0, 1.25,  fx_strobe_rway ,
light.3 = 1, -13.90,  0.0, 0.85,  fx_beacon_rway,
light.4 = 5,  -1.65,  0.0, -1.35,  fx_landing,
light.6 = 4,   -6.0,  0.0, 1.30,  fx_vclighth ,



[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

[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.
//NOTE: These map to cyclic (fore/aft), cyclic (left/right), and anti-torque
elevator = 100,  180
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 = 0
direction_indicator.0=3,0

[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


[fuel]
Center1  = -8.33, 0.0, 0.0, 17.0, 0.5         //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)
fuel_type = 1                                   //Fuel type: 1 = Avgas, 2 = JetA
number_of_tank_selectors = 1                   
electric_pump=1

[GeneralEngineData]
engine_type = 0                                 //0=Piston, 1=Jet, 2=None, 3=Helo-Turbine, 4=Rocket, 5=Turboprop
Engine.0 = -8.5, 0.0, 0.0                        //(feet) longitudinal, lateral, vertical distance from reference datum
fuel_flow_scalar= 4.0                           //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
cylinder_displacement= 40.5                     //Cubic inches per cylinder
compression_ratio= 8.5                          //Compression ratio
number_of_cylinders=4                           //Number of cylinders
max_rated_rpm= 2700                             //Max rated RPM
max_rated_hp= 155                               //Max rated HP
fuel_metering_type= 0                           //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= 1                        //Automixture available? 0=FALSE, 1=TRUE
auto_ignition= 1                                //Auto-Ignition available? 0=FALSE, 1=TRUE
max_rpm_mechanical_efficiency_scalar= 1.0       //Scalar on maximum RPM mechanical efficiency
idle_rpm_mechanical_efficiency_scalar= 1.0      //Scalar on idle RPM mechanical efficiency
max_rpm_friction_scalar= .69                    //Scalar on maximum RPM friction
idle_rpm_friction_scalar= .50                   //Scalar on idle RPM friction

[Reference Speeds]
cruise_speed            = 93.0                 //Knots True (KTAS)
max_indicated_speed     = 130.0                  //Red line (KIAS)

[autopilot]
autopilot_available= 0
flight_director_available= 0

[yaw_string]
yaw_string_available=1

[Helicopter]
reference_length       = 21.58   
reference_frontal_area = 17.7
reference_side_area    = 44.5
side_aero_center       = -12.5
right_trim_scalar      = 1.0
correlator_available   = 1
governed_pct_rpm_ref   = 1.04
governor_pid = 0.4, 0, 0.1, 0, 0.2
rotor_brake_scalar     = 1.5
torque_scalar          = -1.5
cyclic_roll_control_scalar  =2.3
cyclic_pitch_control_scalar =2.4
pedal_control_scalar        =.50
collective_on_rotor_torque_scalar = 0.37

[fuselage_aerodynamics]
drag_force_cf      = 0.55
side_drag_force_cf = 10.0
pitch_damp_cf      = -5.0
roll_damp_cf       = -5.0
yaw_damp_cf        = -0.1
yaw_stability_cf   = 0.19

[MainRotor]
Position = -8.33, 0, 4.61                       //Longitudinal, Lateral, Vertical feet from datum
Radius   = 12.5                               //feet
max_disc_angle = 5.0
RatedRpm = 520
Number_of_blades = 2
Weight_per_blade = 21.0
Weight_to_moi_factor = 0.56
inflow_vel_reference = 32.0
[SecondaryRotor]
Position = -22.8, .660, .850                    //Longitudinal, Lateral, Vertical feet from datum
TailRotor = 1
Radius   = 2.09375                                 //feet

[exits]
number_of_exits=3
exit_rate.0=0.2

[effects]
wake = fx_wake
water = fx_spray
dirt = fx_tchdrt
concrete = fx_sparks
startup =fx_engstrt_RWay
landrotorwash=fx_rtr_lnd_RWay
waterrotorwash=fx_rtr_wtr_RWay
windshield_rain_effect_available=1

[SMOKESYSTEM]
//?,long,lat from ref datum