[fltsim.0]
title=TL-96 Star
sim=Star
model=
panel=
sound=
sound_alias = c172\sound
texture=
kb_checklists=
kb_reference=
atc_id=OH-U666
ui_manufacturer=TL Ultralight
ui_type=TL-96 Star
ui_variation=
description=An ultralight plane from TL Ultralight
atc_heavy=0
atc_airline=
atc_flight_number=
[General]
atc_type=
atc_model=
performance=Maximum Speed\t145 kts\nCruise Speed\t140 kts\nMaximum Range\t820 nm\nService Ceiling\t18,100 ft\nFuel Capacity\t88 U.S gal\nMax Gross Weight\t3,110 lb\nSeating\t\t4\nUseful Load\t1,228 lb\n
[WEIGHT_AND_BALANCE]
max_gross_weight = 2300.000
empty_weight = 1500.000 //oli 650
reference_datum_position = 0.000, 0.000, 0.000
empty_weight_CG_position = 0.300, 0.000, 0.000
max_number_of_stations = 50
station_load.0 =176.000000, 1.000000, -1.000000, 0.000000, longitudinal
station_load.1 =0.000000, 0.000000, 0.000000, 0.000000, longitudinal
station_load.2 =0.000000, -9.600000, -1.500000, 0.000000, longitudinal
station_load.3 = 0, -6.2, 1.5, 0.0 //Rear Passenger Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.4 = 0, -8.0, 0.0, 0.0 //Baggage Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
empty_weight_roll_MOI=700.000000
empty_weight_pitch_MOI=1000.000000
empty_weight_yaw_MOI=1900.000000
empty_weight_coupled_MOI=0.000000
[contact_points]
point.0 = 1.000, 4.000, 0.000, -4.000, 1500.000, 0.000, 0.700, 22.000, 0.250, 2.500, 0.700, 0.000, 0.000, 0.000, 0.000, 0.000
point.1 = 1.000, -1.000, -3.000, -4.000, 3500.000, 1.000, 0.700, 0.000, 0.300, 2.500, 0.700, 0.000, 0.000, 2.000, 0.000, 0.000
point.2 = 1.000, -1.000, 3.000, -4.000, 3500.000, 2.000, 0.700, 0.000, 0.300, 2.500, 0.700, 0.000, 0.000, 3.000, 0.000, 0.000
point.3 = 2.000, -0.300, -15.000, 0.000, 1800.000, 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, -0.300, 15.000, 0.000, 1800.000, 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, -14.000, 0.000, 0.300, 1800.000, 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, 5.080, 0.000, -2.170, 1800.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 4.000, 0.000, 0.000
point.7= 2.000, -19.200, 0.000, 5.830, 1800.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 7.000, 0.000, 0.000
point.8= 2.000, -1.300, 0.000, -2.000, 1800.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 8.000, 0.000, 0.000
max_number_of_points = 21
static_pitch=3.823242
static_cg_height=3.015259
[brakes]
parking_brake = 1 //Parking brake available
toe_brakes_scale = 0.5 //Brake scalar
[Views]
eyepoint= 2, -0.8, 0.5 //(feet) longitudinal, lateral, vertical distance from reference datum
[LIGHTS]
//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit
light.0 = 3, 3.0, -15.3, 0.2, fx_navred
light.1 = 3, 3.0, 15.3, 0.2, fx_navgre
light.2 = 2, 4.5, -15.3, 0.2, fx_strobe
light.3 = 2, 4.5, 15.3, 0.2, fx_strobe
light.4 = 1, -9.2, 0.00, 3.93, fx_beacon
[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
turn_indicator.0=1,1 //Turn AND Bank
direction_indicator.0=1,0
[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=1,0
[EFFECTS]
wake=fx_wake
water=fx_spray
dirt=fx_tchdrt
concrete=fx_sparks
touchdown=fx_tchdwn_s, 1
[fuel]
LeftMain = 0.000, 0.000, 0.000, 0.000, 0.000
RightMain = 0.000, 0.000, 0.000, 0.000, 0.000
fuel_type = 1 //Fuel type: 1 = Avgas, 2 = JetA
number_of_tank_selectors = 1
electric_pump=1
Center1= 1.000, 0.000, 0.000, 15.000, 0.000
[airplane_geometry]
wing_area = 131.000
wing_span = 30.000
wing_root_chord = 5.000
wing_dihedral = 4.000
wing_incidence = 1.500
wing_twist = -1.000
oswald_efficiency_factor= 0.680
wing_winglets_flag = 0
wing_sweep = 0.000
wing_pos_apex_lon = 1.000
wing_pos_apex_vert = 0.000
htail_area = 20.000
htail_span = 7.000
htail_pos_lon = -3.000
htail_pos_vert = 0.000
htail_incidence = 0.000
htail_sweep = 0.000
vtail_area = 18.000
vtail_span = 4.600
vtail_sweep = 60.000
vtail_pos_lon = -7.000
vtail_pos_vert = 0.000
elevator_area = 20.000
aileron_area = 8.000
rudder_area = 8.000
elevator_up_limit = 28.000
elevator_down_limit = 21.000
aileron_up_limit = 20.000
aileron_down_limit = 15.000
rudder_limit = 24.000
elevator_trim_limit = 19.500
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 = 54.000
full_flaps_stall_speed = 43.200
cruise_speed = 110.000
max_indicated_speed= 163.000
[autopilot]
autopilot_available= 0
flight_director_available= 0
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= 8.000
[forcefeedback]
gear_bump_nose_magnitude=6000 ; 0 - 10000
gear_bump_nose_direction=18000 ; 0 - 35999 degrees
gear_bump_nose_duration=250000 ; in microseconds
gear_bump_left_magnitude=6000 ; 0 - 10000
gear_bump_left_direction=35500 ; 0 - 35999 degrees
gear_bump_left_duration=250000 ; in microseconds
gear_bump_right_magnitude=6000 ; 0 - 10000
gear_bump_right_direction=00500 ; 0 - 35999 degrees
gear_bump_right_duration=250000 ; in microseconds
ground_bumps_magnitude1=3250 ; 0 - 10000
ground_bumps_angle1=8900 ; 0 - 35999 degrees
ground_bumps_intercept1=5.0
ground_bumps_slope1=0.48
ground_bumps_magnitude2=750 ; 0 - 10000
ground_bumps_angle2=9100 ; 0 - 35999 degrees
ground_bumps_intercept2=0.075
ground_bumps_slope2=1.0
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= 0.500
extending-time= 7.000
system_type= 0
damaging-speed= 65.000
blowout-speed= 100.000
lift_scalar= 1.000
drag_scalar= 1.000
pitch_scalar= 1.000
flaps-position.0= 0.000, 0.000
flaps-position.1= 10.000, 0.000
flaps-position.2= 25.000, 0.000
[GeneralEngineData]
engine_type=0
Engine.0=4.333333,0.000000,0.000000
fuel_flow_scalar=1.000000
min_throttle_limit=0.000000
[piston_engine]
max_rpm_mechanical_efficiency_scalar=1.00000
idle_rpm_mechanical_efficiency_scalar=1.00
max_rpm_friction_scalar=1.0000
idle_rpm_friction_scalar=1.000000
cylinder_displacement=90.000000
compression_ratio=10.500000
number_of_cylinders=4
max_rated_rpm=5800.000000
max_rated_hp=100.000000
fuel_metering_type=0
cooling_type=0
normalized_starter_torque=0.300000
turbocharged=0
max_design_mp=0.000000
min_design_mp=0.000000
critical_altitude=0.000000
emergency_boost_type=0
emergency_boost_mp_offset=0.000000
emergency_boost_gain_offset=0.000000
fuel_air_auto_mixture=0
auto_ignition=0
[propeller]
propeller_type=1
propeller_diameter=6.333000
propeller_blades=3
propeller_moi=5.000000
beta_max=0.000000
beta_min=0.000000
min_gov_rpm=0.000000
prop_tc=0.000000
gear_reduction_ratio=1.000000
fixed_pitch_beta=20.000000
low_speed_theory_limit=80.000000
prop_sync_available=0
prop_deice_available=0
prop_reverse_available=0.000000
minimum_on_ground_beta=0.000000
minimum_reverse_beta=0.000000
[hydraulic_system]
normal_pressure=0.000000
[flight_tuning]
cruise_lift_scalar=1.0
pitch_stability=1.6
roll_stability=1.2
yaw_stability=1.0
parasite_drag_scalar=1.0
induced_drag_scalar=1.0
elevator_effectiveness=1.3
aileron_effectiveness=1.0
rudder_effectiveness=1.000
elevator_trim_effectiveness=1.8
aileron_trim_effectiveness=1.000
rudder_trim_effectiveness=1.000
