[fltsim.0]
title=Boomerang - Original
sim=Boomerang
model=
panel=
sound=
texture=
sound_alias = beech_baron_58\sound
kb_checklists=
kb_reference=
atc_id=N24BT
ui_manufacturer=Scaled Composites
ui_type=Boomerang
ui_variation=Rutan Model 202
description=Designed by aeronautic geniuses Burt Rutan & John Roncz, the 'Boomerang' is named for it's revolutionary foward-swept assymetric wing. From a starting point based on the Beechcraft Baron, Burt & John proceeded to fix all of the aerodynamic mistakes in conventional twin design and came up with what is one of the most beautiful aircraft ever built. The version is based on the Boomerang as displayed at the EAA Airventure Fly-In at Oshkosh in 1996.
atc_heavy=0
atc_airline=
atc_flight_number=

[fltsim.1]
title=Boomerang - Custom
sim=Boomerang
model=1
panel=
sound=
texture=1
sound_alias = beech_baron_58\sound
kb_checklists=
kb_reference=
atc_id=N24BT
ui_manufacturer=Scaled Composites
ui_type=Boomerang
ui_variation=Rutan Model 202/A - Custom Interior
description=The Boomerang, being a prototype, has a fairly sparse interior. This is my version of an interior for it, with full night light effects. For best results, switch off the cockpit and cabin floodlights for a more subdued night-time flight. Switch on the autopilot and crawl aft for a game on the PS2, feed 'Haku' the goldfish or just relax and watch the LavaLamp!
atc_heavy=0
atc_airline=
atc_flight_number=

[General]
editable=1
atc_type=EXPERIMENTAL
atc_model=R202
performance=Weight Empty\t\t2370 lbs\nMaximum Fuel\t\t1007 lbs\nMaximum Payload\t\t865 lbs\nMaximum Gross Weight\t4242 lbs\n\nSpan\t\t\t36.7 ft\nLength\t\t\t30.6 ft\nWing Area\t\t\t101.7 sq.ft\n\nVmax\t\t283 kts @ 18,000 ft\nCruise\t\t264 kts @ 22,000 ft\nEconomy\t\t210 kts @ 24,000 ft\n\nStall\t\t88 kts @ 4200 lbs\n\t\t77 kts @ 2800 lbs\n\nRange\t\t1500 Nm cruise\n\t\t2100 Nm economy\nincludes takeoff, landing, 45 min reserve\n\n


[WEIGHT_AND_BALANCE]
max_gross_weight = 4242.000
empty_weight = 2370.000

reference_datum_position     = 0.000, 0.000, 0.000
empty_weight_CG_position     = -0.200, 0.000, 0.000

max_number_of_stations = 6

station_load.0 =170.000000, 1.882000, 1.200000, 0.000000, Pilot          
station_load.1 =170.000000, 1.882000, -1.200000, 0.000000, Co-Pilot       
station_load.2 =170.000000, -1.840000, 1.200000, 0.000000, Passenger      
station_load.3 =170.000000, -1.840000, -1.200000, 0.000000, Passenger         
station_load.4 =170.000000, -3.710000, 0.000000, 0.000000, Passenger      
station_load.5 =150.000000, -4.040000, 0.000000, 0.000000, Baggage        

;Moments of Inertia
empty_weight_pitch_MOI  = 3500.000
empty_weight_roll_MOI   = 4500.000
empty_weight_yaw_MOI    = 6500.000
empty_weight_coupled_MOI= 0.000
CG_forward_limit= 0.000
CG_aft_limit= 1.000

[flight_tuning]
cruise_lift_scalar     =1.000
parasite_drag_scalar   =0.352
induced_drag_scalar    =0.602
elevator_effectiveness =1.101
aileron_effectiveness  =1.101
rudder_effectiveness   =1.000
pitch_stability        =1.500
roll_stability         =1.802
yaw_stability          =1.802
elevator_trim_effectiveness =1.000
aileron_trim_effectiveness  =1.000
rudder_trim_effectiveness   =1.052
hi_alpha_on_roll = 0.5
hi_alpha_on_yaw = 0.4
p_factor_on_yaw = 0.05
torque_on_roll = 0.05
gyro_precession_on_roll = 0.2
gyro_precession_on_yaw = 0.2

[GeneralEngineData]
engine_type = 0
Engine.0 = 2.000, -2.610, 0.000
Engine.1 = 2.000, 2.610, 0.000
fuel_flow_scalar= 0.750
min_throttle_limit =  0.0;                      //Minimum percent throttle.  Generally negative for turbine reverser
max_contrail_temperature = -32.0

[piston_engine]
power_scalar =1.000
cylinder_displacement= 91.700
compression_ratio= 8.500
number_of_cylinders= 4
max_rated_rpm= 2700.000
max_rated_hp= 270.819
fuel_metering_type= 0
cooling_type= 0
normalized_starter_torque= 0.150
turbocharged= 1
max_design_mp= 42.000
min_design_mp= 1.000
critical_altitude= 25000.000
emergency_boost_type= 0
emergency_boost_mp_offset= 0.000
emergency_boost_gain_offset= 0.000
fuel_air_auto_mixture= 1
auto_ignition= 1
max_rpm_mechanical_efficiency_scalar=1.000
idle_rpm_mechanical_efficiency_scalar=1.000
max_rpm_friction_scalar=1.000
idle_rpm_friction_scalar=1.000

[propeller]
thrust_scalar =1.000
propeller_type= 0
propeller_diameter= 6.400
propeller_blades= 3
propeller_moi= 6.900
beta_max= 45.000
beta_min= 15.200
min_gov_rpm= 1100.000
prop_tc= 0.100
gear_reduction_ratio= 1.000
fixed_pitch_beta= 0.000
low_speed_theory_limit= 80.000
prop_sync_available= 1
prop_deice_available= 1
prop_feathering_available= 1
prop_auto_feathering_available= 1
min_rpm_for_feather= 700.000
beta_feather= 82.500
power_absorbed_cf= 0.900
defeathering_accumulators_available= 0
feathering_switches = 1
prop_reverse_available= 0.000
minimum_on_ground_beta= 0.000
minimum_reverse_beta= 0.000

[contact_points]
//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
        //14 Airspeed limit for retraction (KIAS)
        //15 Airspeed that gear gets damage at (KIAS)
//GEAR
point.0 = 1.000, 7.174, 0.000, -4.061, 4500.000, 0.000, 0.520, 30.000, 0.305, 1.100, 0.600, 3.000, 3.000, 0.000, 152.000, 180.000
point.1 = 1.000, -0.997, -4.637, -4.061, 2000.000, 1.000, 0.520, 0.000, 0.310, 1.490, 0.870, 4.100, 4.300, 2.000, 152.000, 200.000
point.2 = 1.000, -3.585, 2.611, -4.100, 2000.000, 2.000, 0.520, 0.000, 0.300, 1.700, 0.960, 4.300, 4.100, 3.000, 152.000, 200.000
//SCRAPES
point.3= 2.000, 0.760, -18.910, 0.500, 800.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 5.000, 0.000, 0.000
point.4= 2.000, 0.760, 18.910, 0.500, 800.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 6.000, 0.000, 0.000
point.5= 2.000, -17.080, 0.000, -0.500, 800.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 9.000, 0.000, 0.000
point.6= 2.000, 6.960, 0.000, -1.240, 800.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 4.000, 0.000, 0.000

static_pitch = 0.000
static_cg_height = 3.756
gear_system_type=0              //Electric
max_number_of_points = 7

[gear_warning_system]
gear_warning_available = 1    //Normal
pct_throttle_limit =  0.1     //Percent throttle that activates warning
flap_limit_idle    =  0.0     //Flap angle that activates warning at idle
flap_limit_power   = 16.0     //Flap angle that activates warning at above idle

[brakes]
parking_brake = 1       //Parking brake available
toe_brakes_scale = 1.0  //Brake scalar

[hydraulic_system]
normal_pressure = 3000.0    //PSI
electric_pumps  = 0         //no electric pumps
engine_map      = 1,1,0,0   //pumps on Eng1,2


[electrical]
max_battery_voltage = 24.0
generator_alternator_voltage = 28.0
max_generator_alternator_amps = 60.0

                ;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

[pitot_static]
vertical_speed_time_constant = 1.0              //Increasing this value will cause a more instantaneous reaction in the VSI


[exits]
number_of_exits = 3
exit_rate.0 = 0.3                               ;Percent per second
exit_rate.1 = 0.25                               ;Percent per second
exit_rate.2 = 0.2                               ;Percent per second


[Radios]
// Radio Type = availiable, standby frequency, has glide slope
// Corrected on 30/11/2004
Audio.1=1 
Com.1=1, 0
Com.2=1, 0
Nav.1=1, 0, 1
Nav.2=1, 0, 0
Adf.1=1
Transponder.1=1 
Marker.1=1 

[Views]
eyepoint = 1.55, 3.12, 1.6    //Longitudinal, Lateral, Vertical (feet)

[LIGHTS]
//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing, 10=cabin
light.0 = 3,    1.43, -19.019,  1.262, fx_navred ,
light.1 = 3,   3.265,  18.854,  1.259, fx_navgre ,
light.2 = 3, -19.993,   2.547,  0.683, fx_navwhi ,
light.3 = 2,    1.43, -19.019,  1.262, fx_strobe ,
light.4 = 2,   3.265,  18.854,  1.259, fx_strobe ,
light.5 = 1,  -1.077,   2.548,  2.657, fx_beacon_bm ,
light.6 = 2,   1.542,   2.548, -1.805, fx_strobe ,
light.7 = 10,  -3.645,   2.548,  2.098, fx_vclightwhibm ,
light.8 = 4,    1.00,   2.548,  2.098, fx_vclightbm ,
light.9 = 9,   -15.951, 2.838,  1.066, fx_navwhi ,
light.10 = 9,  -15.787, -4.941, 0.896, fx_navwhi ,


[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

[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 = 1 

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

[fuel]
LeftMain  = -1.500, -6.450, 0.000, 57.000, 0.000
RightMain = -1.500, 6.450, 0.000, 57.000, 0.000
Center1= -1.000, 0.000, 0.000, 57.000, 0.000
fuel_type = 1                                //Fuel type: 1 = Avgas, 2 = JetA
number_of_tank_selectors = 2                    
electric_pump=1



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

[airplane_geometry]
wing_area               = 199.000
wing_span               = 37.800
wing_root_chord         = 5.300
wing_dihedral           = 6.900
wing_incidence          = 0.250
wing_twist              = -2.000
oswald_efficiency_factor= 0.990
wing_winglets_flag      = 0
wing_sweep              = 0.000
wing_pos_apex_lon       = 0.550
wing_pos_apex_vert      = 0.000
htail_area              = 60.000
htail_span              = 15.900
htail_pos_lon           = -13.140
htail_pos_vert          = 0.000
htail_incidence         = 0.250
htail_sweep             = 0.000
vtail_area              = 65.000
vtail_span              = 14.000
vtail_sweep             = 10.000
vtail_pos_lon           = -18.940
vtail_pos_vert          = 0.000
elevator_area           = 20.000
aileron_area            = 11.300
rudder_area             = 10.500
elevator_up_limit       = 17.000
elevator_down_limit     = 15.500
aileron_up_limit        = 18.000
aileron_down_limit      = 18.000
rudder_limit            = 30.000
elevator_trim_limit     = 15.000
spoiler_limit           = 0.000
spoilerons_available    = 0
aileron_to_spoileron_gain = 0.000
min_ailerons_for_spoilerons = 0.000
min_flaps_for_spoilerons = 0.000


[Reference Speeds]
flaps_up_stall_speed    = 88.000
full_flaps_stall_speed  = 73.000
cruise_speed            = 350.000
max_indicated_speed=283.000000
max_mach = 0.65

[autopilot]
autopilot_available= 1
flight_director_available= 1
default_vertical_speed= 700.0
autothrottle_available= 0
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=9.00
nav_integrator_control=0.25
nav_derivative_control=0.00
nav_integrator_boundary=2.50
nav_derivative_boundary=0.00
gs_proportional_control=9.52
gs_integrator_control=0.26
gs_derivative_control=0.00
gs_integrator_boundary=0.70
gs_derivative_boundary=0.00
yaw_damper_gain = 1.0
pitch_takeoff_ga=8.000000

[forcefeedback]
stick_shaker_magnitude=5000             ; 0 - 10000
stick_shaker_direction=0                ; 0 - 35999 degrees
stick_shaker_period=111111              ; in microseconds
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=9000           ; 0 - 35999 degrees
gear_bump_left_duration=250000          ; in microseconds
gear_bump_right_magnitude=2700          ; 0 - 10000
gear_bump_right_direction=27000         ; 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=1

[Flaps.0]
type= 1
span-outboard= 0.800
extending-time= 2.000
system_type= 0
damaging-speed= 165.000
blowout-speed= 250.000
lift_scalar= 1.000
drag_scalar= 1.000
pitch_scalar= 1.000
flaps-position.0= 0.000, 0.000
flaps-position.1= 15.000, 0.000
flaps-position.2= 30.000, 0.000