[fltsim.0]
title=Titanic
sim=Titanic
model=
panel=
sound=
texture=
atc_parking_types=DOCK
ui_manufacturer=Harland and Wolff
ui_type=Olympic Class
ui_variation=Titanic
description=The great Titanic !
atc_parking_codes=
[pitot_static]
vertical_speed_time_constant=1
[WEIGHT_AND_BALANCE]
max_gross_weight=70000 // (pounds)
empty_weight=10088 // (pounds)
reference_datum_position=61.0, 0, 0.0 // (feet) distance from FlightSim Reference position: (1/4 chord, centerline, waterline)
empty_weight_CG_position=-120.5, 0,0 // (feet) longitudinal, lateral, vertical distance from specified datum
max_number_of_stations=50
;Moments of Inertia
empty_weight_roll_MOI=13352310
empty_weight_pitch_MOI=24223159
empty_weight_yaw_MOI=39531785
empty_weight_coupled_MOI=0
[fuel]
LeftMain=-96.0, -28.0, -4.0, 12546.0, 0.0 //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)
RightMain=-96.0, 28.0, -4.0, 12546.0, 0.0 //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)
LeftAux=-112.0, -36.5, -3.0, 4482.0, 0.0 //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)
RightAux=-112.0, 36.5, -3.0, 4482.0, 0.0 //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)
LeftTip=-130.0, -73.0, 0.0, 1322.0, 0.0 //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)
RightTip=-130.0, 73.0, 0.0, 1322.0, 0.0 //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)
Center1=-83.5, 0.0, -7.0, 17164.0, 0.0 //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)
Center2=-193.5, 0.0, 6.0, 3300.0, 0.0 //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=5825.0 //Square feet
wing_span=211.4 //Feet
wing_root_chord=48.8 //Feet
wing_dihedral=7.0 //Degrees
wing_incidence=2.0 //Degrees
wing_twist=-1.0 //Degrees
oswald_efficiency_factor=0.68 //Measure of lift effeciency of wing
wing_winglets_flag=1 //Are winglets available?
wing_sweep=37.5 //Degrees, wing leading edge
wing_pos_apex_lon=-58.2 //Feet, longitudinal distance from reference point, negative going aft
wing_pos_apex_vert=0 //Feet, vertical distance from reference point, positive going up
htail_area=1470 //Square feet
htail_span=72.8 //Feet
htail_pos_lon=-210.0 //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=37.5 //Degrees, horizontal tail leading edge
vtail_area=1060 //Square feet
vtail_span=37.1 //Feet, tip to body
vtail_sweep=45.0 //Degrees, vertical tail leading edge
vtail_pos_lon=-198.5 //Feet, longitudinal distance from reference point, negative going aft
vtail_pos_vert=26.1 //Feet, vertical distance from reference point, positive going up
elevator_area=327 //Square feet
aileron_area=225 //Square feet
rudder_area=230 //Square feet
elevator_up_limit=25 //Degrees
elevator_down_limit=15 //Degrees
aileron_up_limit=25 //Degrees
aileron_down_limit=15 //Degrees
rudder_limit=31.5 //Degrees
elevator_trim_limit=20 //Degrees
spoiler_limit=45 //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=140.0 //Knots True (KTAS)
full_flaps_stall_speed=112.0 //Knots True (KTAS)
cruise_speed=23 //Knots True (KTAS)
max_mach=1.0
max_indicated_speed=30 //Red line (KIAS)
//Hydraulic
[flight_tuning]
cruise_lift_scalar=1.0
parasite_drag_scalar=1.9
induced_drag_scalar=1.0
elevator_effectiveness=1.0
aileron_effectiveness=1.0
rudder_effectiveness=1.0
pitch_stability=0
roll_stability=0
yaw_stability=0
elevator_trim_effectiveness=1.0
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=-120, -20, -7 //(feet) longitudinal, lateral, vertical distance from reference datum
Engine.1=-120, 20, -7 //(feet) longitudinal, lateral, vertical distance from reference datum
fuel_flow_scalar=1.0 //Scalar for fuel flow efficiency
min_throttle_limit=-100.0; //Minimum percent throttle. Generally negative for turbine reverser
[TurbineEngineData]
fuel_flow_gain=0.001 //Gain on fuel flow
inlet_area=0.001 //Square Feet, engine nacelle inlet area
rated_N2_rpm=29920 //RPM, second stage compressor rated value
static_thrust=53000 //Lbs, max rated static thrust at Sea Level
afterburner_available=0 //Afterburner available?
reverser_available=1
[jet_engine]
thrust_scalar=1.0
[autopilot]
autopilot_available=0
[contact_points]
;/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)
point.0=2, 10.15, 0.00, 3.600, 5000, 0, 1.40, 10.0, 0.3, 2.5, 0.8, 1.0, 1.0, 0, 175.0, 175.0
point.1=2, -86.40, -6.250, 3.600, 5000, 1, 1.50, 0.0, 0.4, 2.5, 0.8, 0.0, 0.0, 1, 175.0, 175.0
point.2=2, -86.40, 6.250, 3.600, 5600, 2, 1.50, 0.0, 0.4, 2.5, 0.8, 0.0, 0.0, 2, 175.0, 175.0
point.3=4, 0.0, -2.0, -3.4, 5000.0, 0, 2.0, 0.0, 0.5, 2.5, 0.900, 0.0, 0.0, 0, 220, 250
point.4=4, 0.0, 2.0, -3.4, 5000.0, 0, 2.0, 0.0, 0.5, 2.5, 0.900, 0.0, 0.0, 0, 220, 250
point.5=4, -152.0, -15.0, -3.2, 5000.0, 1, 2.0, 10.0, 1.0, 2.0, 0.900, 0.0, 0.0, 2, 220, 250
point.6=4, -152.0, 15.0, -3.2, 5000.0, 2, 2.0, 10.0, 1.0, 2.0, 0.900, 0.0, 0.0, 3, 220, 250
point.7=2, -490.00, 0.00, 3.600, 5000, 0, 1.40, 10.0, 0.3, 2.5, 0.8, 1.0, 1.0, 0, 175.0, 175.0
point.8=2, 390.00, 0.00, 3.600, 5000, 1, 1.50, 0.0, 0.4, 2.5, 0.8, 0.0, 0.0, 1, 175.0, 175.0
static_pitch=-0.0
static_cg_height=3.5
gear_system_type=1 //Hydraulic
static_pitch=-0.0
static_cg_height=-3.5
gear_system_type=1 //Hydraulic
[gear_warning_system]
gear_warning_available=1 //Normal
pct_throttle_limit=0.1 //Percent throttle that activates warning
flap_limit_idle=5.0 //Flap angle that activates warning at idle
flap_limit_power=25.5 //Flap angle that activates warning at above idle
[brakes]
parking_brake=1 //Parking brake available
toe_brakes_scale=1.24 //Brake scalar
[hydraulic_system]
normal_pressure=3000.0 //PSI
electric_pumps=0 //no electric pumps
engine_map=1,1,1,1 //pumps on Eng1,2,3,4
[electrical]
;BusType, MaxAmpLoad, MinVoltage BusTypes:0=MainBus,1=AvionicsBus,2=BatteryBus,3=HotBatteryBus,4-7=Generator/AlternatorBus(1-4)
autopilot=0, 5 , 17.0
avionics_bus=0, 5 , 17.0
avionics=1, 5 , 17.0
gear_warning=0, 2 , 17.0
fuel_pump=0, 5 , 17.0
light_nav=0, 5 , 17.0
light_landing=0, 5 , 17.0
light_taxi=0, 5 , 17.0
light_panel=0, 5 , 17.0
[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
[SMOKESYSTEM]
smoke.1=-20, -101.0, 3.5, fx_Smoke_logo.fx,
smoke.2=-20, -101.0, -3.5, fx_Smoke_logo.fx,
smoke.3=-20, -116.0, 3.5, fx_Smoke_logo.fx,
smoke.4=-20, -116.0, -3.5, fx_Smoke_logo.fx,
smoke.5=0, -211.0, 3.5, fx_Smoke_logo.fx,
smoke.6=0, -211.0, -3.5, fx_Smoke_logo.fx,
smoke.7=0, -226.0, 3.5, fx_Smoke_logo.fx,
smoke.8=0, -226.0, -3.5, fx_Smoke_logo.fx,
smoke.9=0, 10.0, 3.5, fx_Smoke_logo.fx,
smoke.10=0, 10.0, -3.5, fx_Smoke_logo.fx,
smoke.11=0, 17.0, 3.5, fx_Smoke_logo.fx,
smoke.12=0, 17.0, -3.5, fx_Smoke_logo.fx,
smoke.13=0, 101.0, 3.5, fx_Smoke_logo.fx,
smoke.14=0, 101.0, -3.5, fx_Smoke_logo.fx,
smoke.15=0, 116.0, 3.5, fx_Smoke_logo.fx,
smoke.16=0, 116.0, -3.5, fx_Smoke_logo.fx,
[Views]
eyepoint=191.0,25.0,68.0
[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=2
attitude_indicator.1=1
[turn_indicators]
;/Type: 0=None, 1=Electric Gyro, 2= Vacuum Gyro
turn_indicator.0=0,0
[keyboard_response]
rudder=150, 250
[EFFECTS]
wake=fx_wake_l
water=fx_spray_qm2
dirt=fx_tchdrt
concrete=fx_sparks
touchdown=fx_tchdwn, 1
[exits]
number_of_exits=0
[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=2
[General]
performance= \n \n \n \n \n \n
[Flaps.0]
type=1
span-outboard=0.500000
extending-time=7.000000
system_type=0
