// Edit by Rob, March 17 2011, V1.1 for FS9 (compared to V1.0 for FS9):
// - Light.6 (lights section) now coupled to Strobes, to enable external light effects to be forced Off at ExitOpen
// - Spoiler limit (Geometry section), to reduce effect of Spoilers (should they be used)
// - Reduced brakes scale (brakes section), to reduce jitter effect when ParkingBrakes On
// - Repositioned vertical smoke effect (more down)
// - More rigid gear, to allow higher impact at touchdown
// - Increased fuel consumption
[fltsim.0]
title=THUNDERBIRD 2-GA
sim=THUNDERBIRD 2-GA
model=
panel=
sound=
texture=TB2
kb_checklists=
kb_reference=
atc_id=TB2
atc_airline=INTERNATIONAL RESCUE
atc_flight_number=001
ui_manufacturer=1GUZMAN_ARTES
ui_type=THUNDERBIRD 2
ui_variation=TB2-VC
description=THUNDERBIRD 2 - BY LIBARDO GUZMAN - GUZMAN_ARTES"
[General]
atc_type=THUNDERBIRD 2
atc_model=TB2-VC
performance=\nMax Speed: 990 kts (SeaLevel), 1.40 Mach (40.000 ft) \nDate: 15 March 2011
[pitot_static]
vertical_speed_time_constant = 1 //Increasing this value will cause a more instantaneous reaction in the VSI
[WEIGHT_AND_BALANCE]
max_gross_weight = 93000 // (pounds)
empty_weight = 17000 // (pounds)
reference_datum_position = 0, 0, 0 // (feet) distance from FlightSim Reference position: (1/4 chord, centerline, waterline)
empty_weight_CG_position = -5, 0, 0 // (feet) longitudinal, lateral, vertical distance from specified datum
max_number_of_stations = 50
station_load.0 = "170, 41.0, 0.0, 0.0, Pilot"
station_load.1 = "40000, 0.0, 0.0, 0.0, Cargo"
;Moments of Inertia
empty_weight_pitch_MOI = 3172439
empty_weight_roll_MOI = 2262183
empty_weight_yaw_MOI = 3337024
empty_weight_coupled_MOI = 0
[flight_tuning]
cruise_lift_scalar = 1.0
parasite_drag_scalar = 0.2
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 = 1.5
aileron_trim_effectiveness = 1.0
rudder_trim_effectiveness = 1.0
[GeneralEngineData]
engine_type = 1 //0=Piston, 1=Jet, 2=None, 3=Helo-Turbine, 4=Rocket, 5=Turboprop
Engine.0 = 4.75, -20.0, -10.0 //(feet) longitudinal, lateral, vertical distance from reference datum
Engine.1 = 4.75, 20.0, -10.0 //(feet) longitudinal, lateral, vertical distance from reference datum
fuel_flow_scalar = 0.5 //0.2 //Scalar for fuel flow efficiency
min_throttle_limit = 0 //Minimum percent throttle. Generally negative for turbine reverser
max_contrail_temperature = -30 //Temperature (deg C) below which contrails may appear
[TurbineEngineData]
fuel_flow_gain = 0.002 //Gain on fuel flow
inlet_area = 19.6 //Square Feet, engine nacelle inlet area
rated_N2_rpm = 29920 //RPM, second stage compressor rated value
static_thrust = 23500 //Lbs, max rated static thrust at Sea Level
afterburner_available = 0 //Afterburner available?
reverser_available = 0 //Thrust reverser available?
[jet_engine]
thrust_scalar = 1.3
[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=float>
//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]
//0 Class <0=none,1=wheel, 2=scrape, 3=skid, 4=float, 5=waterrudder >
//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)
// 0 1 2 3 4 5 6 7 8 9 10 11 12
point.0=1, 50.00, 0.0, -25.0, 12574.8, 0, 1.442, 80.00, 0.85, 2.5, 0.9, 0, 0
point.1=1, -30.00, 30.0, -25.0, 12574.8, 1, 1.442, 0.00, 0.85, 2.5, 0.9, 0, 0
point.2=1, -30.00, -30.0, -25.0, 12574.8, 2, 1.442, 0.00, 0.85, 2.5, 0.9, 0, 0
point.3= 5, 0.0, 0.0, -7.300, 1600, 0, 0.00, 50.0, 0.0, 0.0, 1.00, 3.0, 3.2, 0, 0.0, 0.0
max_number_of_points = 21
static_pitch=0.0 //degrees, pitch when at rest on the ground (+=Up, -=Dn)
static_cg_height=24.2 //feet, altitude of CG when at rest on the ground
gear_system_type=1 //Hydraulic
[gear_warning_system]
gear_warning_available=0
pct_throttle_limit=0.000000
flap_limit_power=0.000000
flap_limit_idle=0.000000
[brakes]
toe_brakes_scale=0.1 //1.0
parking_brake=1
[hydraulic_system]
normal_pressure=0.000000
[Views]
eyepoint=86.60, 0.0, 5.7 //(feet) longitudinal, lateral, vertical distance from reference datum
[flaps.0] //Visual nozzles only
type = 1
span-outboard = 0.7
extending-time = 0.8
flaps-position.0 = 0
flaps-position.1 = 60
damaging-speed = 1000
blowout-speed = 1000
lift_scalar = 0.0
drag_scalar = 0.0
pitch_scalar= 0.0
system_type = 0
[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
[lights]
//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing
// 6=taxi, 7=recognition, 8=wing, 9=logo, 10=cabin
// Max. 19 entries
light.0 = 9, -100, 20, -10, fx_RCB_SmokeHor, //Smoke Backward
light.1 = 9, -100, -20, -10, fx_RCB_SmokeHor, //Smoke Backward
light.2 = 8, -21, -27.2, -25, fx_RCB_SmokeVert, //Smoke Downward
light.3 = 8, -21, 27.2, -25, fx_RCB_SmokeVert, //Smoke Downward
light.4 = 8, 37, 31, -25, fx_RCB_SmokeVert, //Smoke Downward
light.5 = 8, 37, -31, -25, fx_RCB_SmokeVert, //Smoke Downward
light.6 = 2, -87.40, 0.00, 23.00, fx_navwhih , // 2
light.7 = 2, 30.30, -71.08, -7.00, fx_strobeh ,
light.8 = 2, 30.30, 71.08, -7.00, fx_strobeh ,
light.9 = 2, 30.00, 0.00, -24.20, fx_beaconb ,
light.10 = 1, 30.00, 0.00, 19.00, fx_beaconh ,
light.11 =10, -21, -27.2, -20, fx_Bob_FlameDown, //Flame Downward
light.12 =10, -21, 27.2, -20, fx_Bob_FlameDown, //Flame Downward
light.13 =10, 37, 31.2, -20, fx_Bob_FlameDown, //Flame Downward
light.14 =10, 37, -31.2, -20, fx_Bob_FlameDown, //Flame Downward
light.15 = 7, -100, 20, -10, fx_Bob_BurnerFlame, //Flame Backward
light.16 = 7, -100, -20, -10, fx_Bob_BurnerFlame, //Flame Backward
[SMOKESYSTEM]
smoke.0 = 0,70,0, fx_RCB_machenvlop,
[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]
turn_indicator.0=1,0
[exits]
number_of_exits = 2
exit_rate.0 = 0.025 ;Percent per second
exit_rate.1 = 0.05 ;Percent per second
[EFFECTS]
wake=fx_wake
water=fx_spray
dirt=fx_tchdrt
concrete=fx_sparks
touchdown=fx_tchdwn, 1
startup=fx_rengstrt_propliner
[autopilot]
autopilot_available=1
flight_director_available=1
default_vertical_speed=1800
autothrottle_available=1
autothrottle_arming_required=1
autothrottle_max_rpm = 120
autothrottle_takeoff_ga=1
pitch_takeoff_ga = 8;
max_pitch=1.0
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=12.00
nav_integrator_control=0.25
nav_derivative_control=0.00
nav_integrator_boundary=2.50
nav_derivative_boundary=0.00
gs_proportional_control=25.0
gs_integrator_control=0.53
gs_derivative_control=0.00
gs_integrator_boundary=0.70
gs_derivative_boundary=0.00
yaw_damper_gain = 10.0
default_pitch_mode=0
default_bank_mode=0
[fuel]
Center1 = 0, 0, 0, 2313, 0 //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)
LeftMain = -3, -19, 0, 1500, 0 //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)
RightMain = -3, 19, 0, 1500, 0 //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)
fuel_type = 2 //Fuel type: 1 = Avgas, 2 = JetA
number_of_tank_selectors = 1
electric_pump=0
[airplane_geometry]
wing_area = 1137.0 //Square feet
wing_span = 94.75 //Feet
wing_root_chord = 18.0 //Feet
wing_dihedral = 6.2 //Degrees
wing_incidence = 1.0 //Degrees
wing_twist = -0.5 //Degrees
oswald_efficiency_factor= 0.75 //Measure of lift effeciency of wing
wing_winglets_flag = 0 //Are winglets available?
wing_sweep = 25.0 //Degrees, wing leading edge
wing_pos_apex_lon = 8.0 //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 = 338.0 //Square feet
htail_span = 41.7 //Feet
htail_pos_lon = -35.0 //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 = 30.0 //Degrees, horizontal tail leading edge
vtail_area = 224.0 //Square feet
vtail_span = 20.0 //Feet, tip to body
vtail_sweep = 35.0 //Degrees, vertical tail leading edge
vtail_pos_lon = -35.8 //Feet, longitudinal distance from reference point, negative going aft
vtail_pos_vert = 5.8 //Feet, vertical distance from reference point, positive going up
elevator_area = 70.5 //Square feet
aileron_area = 26.9 //Square feet
rudder_area = 56.2 //Square feet
elevator_up_limit = 22.5 //Degrees
elevator_down_limit = 19.5 //Degrees
aileron_up_limit = 20.0 //Degrees
aileron_down_limit = 20.0 //Degrees
rudder_limit = 26.0 //Degrees
elevator_trim_limit = 20.0 //Degrees
spoiler_limit = 5 //60.0 //Degrees
spoilerons_available = 1 //Spoilerons Available?
aileron_to_spoileron_gain = 3 //Aileron to spoileron gain
min_ailerons_for_spoilerons = 10 //Degrees
min_flaps_for_spoilerons = 0 //Minimum flap handle position when spoilerons activate
[Reference Speeds]
flaps_up_stall_speed = 2000 //Knots True (KTAS)
full_flaps_stall_speed = 2000 //Knots True (KTAS)
cruise_speed= 1152.924
max_indicated_speed=1400.000
max_mach=1.600000 //Red line (KIAS)
[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
[TailHook]
tailhook_length=6.8 // feet in longitudinal,lateral,vertical positions -> datum
tailhook_position=0.0, 0.0, -0.0,
cable_force_adjust=0.0
