//***************************************
//* C4-SST v 1.0 AIRCRAFT CONFIGURATION *
//*     For Flight Simulator 2002       *
//*    Copyright© 2002 By Nick Pike     *
//*        All Rights Reserved          *
//***************************************
[fltsim.0]
title=C4-SST v 1.0
sim=C4SST
model=
panel=
sound=
texture=
kb_checklists=C4-SST_check
kb_reference=C4-SST_ref
atc_id_enable=1
atc_id=PacAir1
atc_airline=Pacific Air
atc_flight_number=PacAir1
atc_type=BRITISHAEROSPACE
ui_manufacturer=British Aerospace
ui_type=C4SST
ui_variation=Pacific Air Livery
//visual_damage=1
editable=1
description=Fly 10 passengers and 4 crew around the World in idle luxury with Pacific Air versatility at Mach 2.0. Model, Flight Dynamics, Paint by Hawk. 

[General]
atc_type=BRITISHAEROSPACE
atc_model=C4SST
performance=Dimensions \nSPAN = 78 ft\nLENGTH = 107 ft\nWEIGHT = MTOW 94 000 LBS\nWEIGHT = EMPTY 60 000 LBS\n\nCRUISE SPEED = Mach 2 @ 67,000 ft\nRANGE = 8000 miles

[WEIGHT_AND_BALANCE]
reference_datum_position=0.000000,0.000000,0.000000
empty_weight_CG_position=0.000000,0.000000,0.000000
max_number_of_stations=50
station_load.0=0.000000,0.000000,0.000000,0.000000
empty_weight=60000.000000
empty_weight_roll_MOI=1500000.000000
empty_weight_pitch_MOI=3000000.000000
empty_weight_yaw_MOI=2000000.000000
empty_weight_coupled_MOI=0.000000

[flight_tuning]
cruise_lift_scalar=1.0
parasite_drag_scalar=1.0
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=1.0
aileron_trim_effectiveness=1.0
rudder_trim_effectiveness=1.0

[GeneralEngineData]
engine_type=1
Engine.0=-25.000000,-3.333333,-2.500000
Engine.1=-25.000000,3.333333,-2.500000
fuel_flow_scalar=1.000000

[TurbineEngineData]
fuel_flow_gain=0.002000
inlet_area=28.000000
rated_N2_rpm=29920.000000
static_thrust=33000.000000
afterburner_available=1
reverser_available=1

[jet_engine]
thrust_scalar=1.0

//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]
point.0=1.000000,34.166667,0.000000,-14.250000,1652.034249,0.000000,1.403640,25.000000,0.966517,2.500000,0.480802,15.000000,15.000000,0.000000,0.000000,0.000000
point.1=1.000000,-9.166667,-12.916667,-13.666667,1574.803150,1.000000,1.403640,0.000000,0.468321,2.500000,0.690716,16.000000,16.000000,2.000000,0.000000,0.000000
point.2=1.000000,-9.166667,12.916667,-13.666667,1574.803150,2.000000,1.403640,0.000000,0.468321,2.500000,0.690716,16.000000,16.000000,3.000000,0.000000,0.000000
point.3=2.000000,-50.666667,-45.833333,-0.583333,1574.803150,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,5.000000,0.000000,0.000000
point.4=2.000000,-50.666667,45.833333,-0.583333,1574.803150,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,6.000000,0.000000,0.000000
point.5=2.000000,-82.416667,0.000000,2.833333,1574.803150,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,9.000000,0.000000,0.000000
point.6=2.000000,37.333333,0.166667,2.833333,1574.803150,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,4.000000,0.000000,0.000000
static_pitch=0.000000
static_cg_height=13.169918

[Views]
eyepoint=49.500000,-1.883920,1.045657  // was 50.000000  1.345657

[flaps.0]       //Canard
type=1                                    // 1 - tail, 2 - lead
span-outboard=0.4                         // 0.0 .. 1.0
extending-time=30                         // seconds
flaps-position.0=0                        // degrees
flaps-position.1=90                       // degrees
damaging-speed=1500                       // KIAS
blowout-speed=1700                        // KIAS
lift_scalar=1.0
drag_scalar=1.0
pitch_scalar=0.0
system_type=1                             //Hydraulic

[Radios]
// Radio Type=available, 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, 1
Transponder.1=1
Marker.1=1

[keyboard_response]
elevator=150.000000,250.000000
aileron=150.000000,250.000000
rudder=150.000000,250.000000

[direction_indicators]
direction_indicator.0=3,0

[LIGHTS]
//SWITCH Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing, 6=taxi, 7=recognition, 8=wing, 9=Logo       
//LIGHT  Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing, 6= N/A, 7=wheel well , 8=wing, 9=Logo
light.0=4,  50.40,  0.00, 2.30, fx_vclight
light.1=9, -29.00,   15.30, -0.30, fx_navwhi             //Logo light bulbs
light.2=9, -29.00,   -15.30, -0.30, fx_navwhi            //Logo light bulbs
light.3=7, 28.00,  10.00, 2.50, fx_contrail_fog_C4_1.fx  //wing top fog
light.4=7, 28.00, -10.00, 2.50, fx_contrail_fog_C4_1.fx  //wing top fog
light.5=7, 22.00,  15.00, 3.50, fx_contrail_fog_C4_2.fx  //wing top fog
light.6=7, 22.00, -15.00, 3.50, fx_contrail_fog_C4_2.fx  //wing top fog
light.7=7, 16.00,  20.00, 4.50, fx_contrail_fog_C4_3.fx  //wing top fog
light.8=7, 16.00, -20.00, 4.50, fx_contrail_fog_C4_3.fx  //wing top fog
light.9=7, 10.00,  25.00, 5.50, fx_contrail_fog_C4_4.fx  //wing top fog
light.10=7, 10.00, -25.00, 5.50, fx_contrail_fog_C4_4.fx //wing top fog
light.11=8, -30.00, 41.00, 3.00, fx_contrail_tip_C4.fx   //wing tip fog
light.12=8, -30.00, -41.00, 3.00, fx_contrail_tip_C4.fx  //wing tip fog
light.13=5, 57.00, -1.70, -2.40, fx_cplite_C4.fx         //cp landing light
light.14=6, 57.00, -1.70, -2.30, fx_cplite_C4.fx         //cp taxi light


[electrical]
;BusType, MaxAmpLoad, MinVoltage
;BusTypes:0=MainBus,1=AvionicsBus,2=BatteryBus,3=HotBatteryBus,4-7 Generator/AlternatorBus(1-4)     
;The voltage produced by the alternator/generator, in Volts:
generator_alternator_voltage=28

;Voltage of the battery when fully charged. In Volts:
max_battery_voltage=28.0
max_generator_alternator_amps=60.0
flap_motor=0, 0.5 , 17.0
gear_motor=0, 0.5 , 17.0
autopilot=1, 0.2 , 17.0
avionics_bus=0, 0.5 , 17.0
avionics=1, 0.5 , 17.0
pitot_heat=0, 0.2 , 17.0
additional_system=0, 2.0 , 17.0
marker_beacon=1, 0.2 , 17.0
gear_warning=0, 0.2 , 17.0
fuel_pump=0, 0.5 , 17.0
hydraulic_pump=0, 0.3 , 17.0
starter1=0, 2.0 , 17.0
starter2=0, 2.0 , 17.0
light_nav=0, 0.01 , 17.0
light_beacon=0, 0.01 , 17.0
light_landing=0, 0.01 , 17.0
light_taxi=0, 0.01 , 17.0
light_strobe=0, 0.01 , 17.0
light_panel=0, 0.01 , 17.0
light_logo=0, 0.01 , 17.0

[EFFECTS]
wake=fx_wake
water=fx_spray
dirt=fx_tchdrt
concrete=fx_sparks
touchdown=fx_tchdwn, 1
//visual_damage=1

[fuel]
Center1=8.000000,0.000000,0.000000,1645.000000,0.000000
LeftMain=-4.000000,-20.000000,0.000000,1645.000000,0.000000
RightMain=-4.000000,20.000000,0.000000,1645.000000,0.000000
fuel_type=2.000000
number_of_tank_selectors=2

[airplane_geometry]
wing_area=1000.000000
wing_span=56.666667
wing_root_chord=37.500000
wing_dihedral=0.000000
wing_incidence=0.247192
wing_twist=1.999512
oswald_efficiency_factor=1.000000
wing_winglets_flag=0
wing_sweep=0     // was 40.000000
wing_pos_apex_lon=0.000000
wing_pos_apex_vert=0.000000
htail_area=300.000000
htail_span=37.500000
htail_pos_lon=-37.500000
htail_pos_vert=0.000000
htail_incidence=0.000000
htail_sweep=0.000000
vtail_area=350.000000
vtail_span=21.330729
vtail_sweep=30.000000
vtail_pos_lon=-29.166667
vtail_pos_vert=5.833333
elevator_area=10.000000
aileron_area=10.000000
rudder_area=10.000000
elevator_up_limit=26.000825
elevator_down_limit=26.000825
aileron_up_limit=30.000070
aileron_down_limit=30.000070
rudder_limit=30.000070
elevator_trim_limit=19.996227
spoiler_limit=230.000000   //was 220.000000
spoilerons_available=0
aileron_to_spoileron_gain=0.000000
min_ailerons_for_spoilerons=0.000000
min_flaps_for_spoilerons=0.000000

[Reference Speeds]
flaps_up_stall_speed=150.000000
full_flaps_stall_speed=100.000000
cruise_speed=1150.473984

[autopilot]
autopilot_available=1
flight_director_available=1
default_vertical_speed=2000.000000
autothrottle_available=1
autothrottle_arming_required=1
autothrottle_takeoff_ga=1
autothrottle_max_rpm=90.000000 ;tried 110.000000
pitch_takeoff_ga=8.000000
use_no_default_pitch=1 // 0 = Default to current pitch mode, 1 = No default pitch mode.
use_no_default_bank=1 // 0 = Default to Wing Leveler mode, 1 = No default bank mode
autoland_available=1

[pitot_static]
vertical_speed_time_constant=30 // was 10

[SMOKESYSTEM]
//(feet) vertical, longitudinal, lateral
smoke.0= -2.00, -55.00, 3.33, fx_exhaust_C4.fx
smoke.1= -2.00, -55.00, -3.33, fx_exhaust_C4.fx

[forcefeedback]
stick_shaker_magnitude=2000		; 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=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