[fltsim.0]
title=FSDS3 Baja Buggy
sim=FSDS3 Roberts Racing Baja Buggy
model=
panel=
sound=
texture=
kb_checklists=
atc_id=RRDB
ui_manufacturer=Roberts Racing
ui_type=Roberts Racing Baja Buggy
ui_variation=2 Seat Race Ready Racing Buggy
description=Roberts Racing Baja Buggy - 2 Seat, Powered by a Porsche 3.2 Flat 6 engine.
[General]
atc_type=
atc_model=Roberts Racing
editable=0
performance= Horizontaly opposed Porsche Flat six cylinder, Normaly aspirated engine running via four Weber IDE Carburetors, Churning out 250 hp.
[WEIGHT_AND_BALANCE]
max_gross_weight = 20450.0 // (pounds)
empty_weight = 11700.0 // (pounds)
reference_datum_position = 0, 0, 0 // (feet) distance from FlightSim Reference position: (1/4 chord, centerline, waterline)
empty_weight_CG_position = -2, 0, 0 // (feet) longitudinal, lateral, vertical distance from specified datum
max_number_of_stations = 50
station_load.0 = 0.0, 0.0, 0.0, 0.0 //Pilot Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
;Moments of Inertia
empty_weight_pitch_MOI = 4543
empty_weight_roll_MOI = 3543
empty_weight_yaw_MOI = 10000
empty_weight_coupled_MOI = 0.0
[pitot_static]
vertical_speed_time_constant = 5.0 //Increasing this value will cause a more instantaneous reaction in the VSI
[flight_tuning]
cruise_lift_scalar = 0.01
parasite_drag_scalar = 2.5
induced_drag_scalar = 1.0
elevator_effectiveness = 0.1
aileron_effectiveness = 0.1
rudder_effectiveness = 0.5
pitch_stability = 1.0
roll_stability = 1.0
yaw_stability = 2.0
elevator_trim_effectiveness = 0.1
aileron_trim_effectiveness = 0.1
rudder_trim_effectiveness = 0.1
p_factor_on_yaw = -0.16
torque_on_roll = 0.1
gyro_precession_on_yaw = 0.5
gyro_precession_on_pitch = 0.5
[GeneralEngineData]
engine_type = 0 //0=Piston, 1=Jet, 2=None, 3=Helo-Turbine, 4=Rocket, 5=Turboprop
Engine.0 = -2.0, 0.0, 0.0 //(feet) longitudinal, lateral, vertical distance from reference datum
fuel_flow_scalar= 0.33 //Fuel flow scalar
min_throttle_limit = 0.0 //Minimum percent throttle. Generally negative for turbine reverser
[piston_engine]
power_scalar = 1.3 //Piston power scalar
cylinder_displacement= 90.3 //Cubic inches per cylinder
compression_ratio= 8.0 //Compression ratio
number_of_cylinders=12 //Number of cylinders
max_rated_rpm= 5500.0 //Max rated RPM
max_rated_hp= 450 //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= 1 //Is it turbocharged? 0=FALSE, 1=TRUE
max_design_mp= 48 //Max design manifold pressure, (inHg)
min_design_mp= 1 //Min design manifold pressure, (inHg)
critical_altitude= 0.0 //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= 0 //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= 1.0 //Scalar on maximum RPM friction
idle_rpm_friction_scalar= 1.0 //Scalar on idle RPM friction
[propeller]
thrust_scalar = 1.3 //Propeller thrust scalar
propeller_type= 0 //0=Constant Speed, 1=Fixed Pitch
propeller_diameter= 6.333 //Propeller Diameter, (feet)
propeller_blades= 4 //Number of propeller blades
propeller_moi= 8.0 //Propeller moment of inertia
beta_max= 43 //Maximum blade pitch angle for constant speed prop, (degrees)
beta_min= 10 //Minimum blade pitch angle for constant speed prop, (degrees)
min_gov_rpm= 1400 //Miminum governed RPM
prop_tc= 0.1 //Prop time-constant
gear_reduction_ratio= 1.0 //Propeller gear reduction ratio
fixed_pitch_beta= 20 //Fixed pitch angle of fixed pitch prop, (degrees)
low_speed_theory_limit= 80 //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 //Feathering pitch angle (degrees)
power_absorbed_cf= 0 //Coefficient of friction for power absorbed by propeller
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)
[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, 2 , 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
//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, -4.000, 0.000, -2.277, 1574.8, 0, 0.790, -6.00, 0.266, 2.1 0.966, 0.0, 0.0, 0, 0.0, 0.0
point.1=1, 4.8, -4.377, -2.287, 1574.8, 0, 0.69, 30.0, 0.296, 2.1, 0.866, 0.0, 0.0, 0, 0.0, 0.0
point.2=1, 4.8, 4.377, -2.287, 1574.8, 0, 0.69, 30.0, 0.296, 2.1, 0.866, 0.0, 0.0, 0, 0.0, 0.0
point.3=1, -5.8, -4.377, -2.287, 1574.8, 1, 0.789, 0.00, 0.296, 2.2, 0.866, 0.0, 0.0, 2, 0.0, 0.0
point.4=1, -5.8, 4.377, -2.287, 1574.8, 2, 0.789, 0.00, 0.296, 2.2, 0.866, 0.0, 0.0, 3, 0.0, 0.0
point.5=2, 7.308, -4.395, -0.79, 1574.8, 0, 0.000, 0.00, 0.000, 0.0, 0.000, 0.0, 0.0, 5, 0.0, 0.0
point.6=2, 7.308, 4.395, -0.79, 1574.8, 0, 0.000, 0.00, 0.000, 0.0, 0.000, 0.0, 0.0, 6, 0.0, 0.0
point.7=2, -7.248, -4.395, 0.0, 1574.8, 0, 0.000, 0.00, 0.000, 0.0, 0.000, 0.0, 0.0, 9, 0.0, 0.0
point.8=2, -7.248, 4.395, 0.0, 1574.8, 0, 0.000, 0.00, 0.000, 0.0, 0.000, 0.0, 0.0, 4, 0.0, 0.0
point.9=2, 0.0, -2.395, 0.0, 1574.8, 0, 0.000, 0.00, 0.000, 0.0, 0.000, 0.0, 0.0, 7, 0.0, 0.0
point.10=2, 0.0, 2.395, 0.0, 1574.8, 0, 0.000, 0.00, 0.000, 0.0, 0.000, 0.0, 0.0, 8, 0.0, 0.0
max_number_of_points = 21
static_pitch = 0.0
static_cg_height = 2.0
gear_system_type=0 //Electric
[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 = 3.0 //Brake scalar
differential_braking_scale = 2.0
[hydraulic_system]
normal_pressure = 3000.0 //PSI
electric_pumps = 0 //no electric pumps
engine_map = 1,0,0,0 //pumps on Eng1
[Views]
eyepoint = 0.0, 2.20, 6.26
[flaps.0]
type = 1 // 1 - tail, 2 - lead
span-outboard = 0.5 // 0.0 .. 1.0
extending-time = 15 // seconds
flaps-position.0 = 0 // degrees, KIAS
flaps-position.1 = 8 // degrees, KIAS
flaps-position.2 = 33 // degrees, KIAS
flaps-position.3 = 45 // degrees, KIAS
flaps-position.4 = 90 // degrees, KIAS
damaging-speed = 250 // KIAS
blowout-speed = 300 // KIAS
lift_scalar = -1.0
drag_scalar = 2.0
pitch_scalar= 1.0
system_type = 0 //0=Electric, 1=Hydraulic, 2=Pneumatic, 3=Manual, 4=None
[Radios]
// Radio Type = availiable, standby frequency, has glide slope
Audio.1 = 1
Com.1 = 1, 0
Com.2 = 1, 0, 0
Nav.1 = 0, 0, 0
Nav.2 = 0, 0, 0
Adf.1 = 1
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 = 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 = 4
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=1,0
[EFFECTS]
//dirt=fx_tchdrt
//concrete=fx_sparks
//touchdown=fx_tchdwn_s, 1
[fuel]
LeftMain = -0.3, -0.30, -0.3, 27.5, 0.0 //for air file match.cb
RightMain =-0.3, 0.30, -0.3, 27.5, 0.0
fuel_type = 1 //Fuel type: 1 = Avgas, 2 = JetA
number_of_tank_selectors = 1
electric_pump=1
[airplane_geometry]
wing_area = 0.0 //Square feet
wing_span = 0.0 //Feet
wing_root_chord = 0.0 //Feet
wing_dihedral = 0.0 //Degrees
wing_incidence = 0.0 //Degrees
wing_twist = 0.0 //Degrees
oswald_efficiency_factor= 0.0 //Measure of lift effeciency of wing
wing_winglets_flag = 0.0 //Are winglets available?
wing_sweep = 0.0 //Degrees, wing leading edge
wing_pos_apex_lon = 0.0 //Feet, longitudinal distance from reference point, negative going aft
wing_pos_apex_vert = 0.0 //Feet, vertical distance from reference point, positive going up
htail_area = 0.0 //Square feet
htail_span = 0.0 //Feet
htail_pos_lon = 0.0 //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 = 0.0 //Degrees, horizontal tail leading edge
vtail_area = 10.0 //Square feet
vtail_span = 3.6 //Feet, tip to body
vtail_sweep = 0.0 //Degrees, vertical tail leading edge
vtail_pos_lon = -6.0 //Feet, longitudinal distance from reference point, negative going aft
vtail_pos_vert = 0.0 //Feet, vertical distance from reference point, positive going up
elevator_area = 0.0 //Square feet
aileron_area = 0.0 //Square feet
rudder_area = 8.0 //Square feet
elevator_up_limit = 0.0 //Degrees
elevator_down_limit = 0.0 //Degrees
aileron_up_limit = 0.0 //Degrees
aileron_down_limit = 0.0 //Degrees
rudder_limit = 24.0 //Degrees
elevator_trim_limit = 0.0 //Degrees
spoiler_limit = 70.0 //Degrees
spoilerons_available = 1 //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 = 66.0 //Knots True (KTAS)
full_flaps_stall_speed = 52.8 //Knots True (KTAS)
cruise_speed = 195.0 //Knots True (KTAS)
max_indicated_speed=195.000000
[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]
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=1
[exits]
number_of_exits=2
exit_rate.0=0.4
