[fltsim.0]
title=Lockheed Super Constellation
sim=connie
model=
panel=
sound=
texture=
panel_alias =
sound_alias =
kb_checklists=
kb_reference=
atc_id=N6937C
atc_airline=TWA
atc_flight_number=176
ui_manufacturer=Lockheed
ui_type=Super Constellation
ui_variation=TWA, Trans World Airlines "Star of America"       
description=TWA, Lockheed L-1049G Super Constellation, Circa 1959. Tail number N6937C depicting the Save-A-Connie group's restoration of the "Star of America".  Vist their web-site at, http://www.airlinehistorymuseum.com.  Lockheed Constellation model by Mike Stone.  Panel by Jan Visser and Hansjoerg Naegele.  Sounds by Dave McQueen. TWA textures and FS2002 aircraft compilation package by Kevin Sparkuhl.   

[General]
atc_type=Lockheed
atc_model=Coni
atc_heavy=0
editable=1
performance=Cruise Speed: 311 mph\nMaximum Speed: 366 mph\nRange (Max Fuel):4,815 miles\nRange (Max Payload): 4,065 miles\nAverage Fuel Burn: 500 gph\nFuel Capacity: 7,750 US gal\nService Ceiling: 22,800 feet\nEmpty Weight: 73,016 lbs\nMax Takeoff Weight: 137,500 lbs\nMax Landing Weight: 113,000 lbs\nMax Payload: 24,293 lbs\n\nWingspan: 123 ft 5 in\nLength: 116 ft 2 in\nHeight: 24 ft 9in\n\nEngines: Wright R-3350-93 Turbo Compound, (18 cylinders, 36 spark plugs each!!)\nRated Horsepower: 3400 hp each\nPassengers: 53 to 88\nTypical Crew: Captain, First Officer, Flight Engineer, Flight Navigator, Purser and 2-3 Hostesses.\nBuilt in 1958 and delivered in 1959.\n


[WEIGHT_AND_BALANCE]
max_gross_weight = 137500.000
empty_weight = 73016.000

reference_datum_position     = 0.000, 0.000, 0.000
empty_weight_CG_position     = 0.000, 0.000, 0.000

max_number_of_stations =50


;Moments of Inertia
empty_weight_pitch_MOI  = 1512307.698
empty_weight_roll_MOI   = 1688233.422
empty_weight_yaw_MOI    = 3190301.479
empty_weight_coupled_MOI= 0.000
CG_forward_limit= 0.000
CG_aft_limit= 1.000
station_load.0=0.000000,0.000000,0.000000,0.000000

[flight_tuning]
cruise_lift_scalar     =1.101
parasite_drag_scalar   =0.701
induced_drag_scalar    =1.000
elevator_effectiveness =0.512
aileron_effectiveness  =1.398
rudder_effectiveness   =1.000
pitch_stability        =2.002
roll_stability         =1.000
yaw_stability          =1.000
elevator_trim_effectiveness =0.510
aileron_trim_effectiveness  =1.000
rudder_trim_effectiveness   =1.000

[GeneralEngineData]
engine_type = 0
Engine.0 = 4.000, -30.000, 0.000     //(feet) longitudinal, lateral, vertical 
Engine.1 = 6.000, -14.000, -1.500
Engine.2= 6.000, 14.000, -1.500
Engine.3= 4.000, 30.000, 0.000
fuel_flow_scalar = 0.450

[SMOKESYSTEM]
smoke.0 =  0.00, 0.00, -30.00, fx_smoke_rx  //(feet) vertical, longitudinal, lateral
smoke.1 = -1.50, 2.00, -14.00, fx_smoke_rx
smoke.2 = -1.50, 2.00,  14.00, fx_smoke_rx
smoke.3 =  0.00, 0.00,  30.00, fx_smoke_rx

[piston_engine]
power_scalar =1.351
cylinder_displacement= 250.000
compression_ratio= 8.000
number_of_cylinders= 18
max_rated_rpm= 2700.000
max_rated_hp= 3165.000
fuel_metering_type= 0
cooling_type= 0
normalized_starter_torque= 0.300
turbocharged= 0
max_design_mp= 0.000
min_design_mp= 0.000
critical_altitude= 0.000
emergency_boost_type= 0
emergency_boost_mp_offset= 0.000
emergency_boost_gain_offset= 0.000
fuel_air_auto_mixture= 0
auto_ignition= 0
max_rpm_mechanical_efficiency_scalar=1.000
idle_rpm_mechanical_efficiency_scalar=1.000
max_rpm_friction_scalar=1.000
idle_rpm_friction_scalar=1.000

[propeller]
thrust_scalar =1.351
propeller_type= 0
propeller_diameter= 15.000
propeller_blades= 3
propeller_moi= 89.000
beta_max= 45.000
beta_min= 15.200
min_gov_rpm= 1100.000
prop_tc= 0.100
gear_reduction_ratio= 1.000
fixed_pitch_beta= 0.000
low_speed_theory_limit= 80.000
prop_sync_available= 1
prop_deice_available= 1
prop_feathering_available= 1
prop_auto_feathering_available= 0
min_rpm_for_feather= 700.000
beta_feather= 82.500
power_absorbed_cf= 0.900
defeathering_accumulators_available= 0 
prop_reverse_available= 0
minimum_on_ground_beta= 0.000
minimum_reverse_beta= 0.000

[contact_points]
//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
        //14 Airspeed limit for retraction (KIAS)
        //15 Airspeed that gear gets damage at (KIAS)
//GEAR
point.0 = 1.000, 40.000, 0.000, -10.300, 1600.000, 0.000, 0.850, 45.000, 0.300, 2.500, 0.950, 5.000, 5.000, 0.000, 0.000, 0.000
point.1 = 1.000, -3.000, -14.000, -10.400, 1600.000, 1.000, 1.200, 0.000, 0.500, 2.500, 0.950, 5.000, 5.000, 2.000, 0.000, 0.000
point.2 = 1.000, -3.000, 14.000, -10.400, 1600.000, 2.000, 1.200, 0.000, 0.500, 2.500, 0.950, 5.000, 5.000, 3.000, 0.000, 0.000
//SCRAPES
point.3= 2.000, 0.000, -62.900, 5.430, 800.000, 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, 0.000, 62.900, 5.430, 800.000, 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, -65.490, 0.000, 4.880, 800.000, 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, 47.540, 0.000, 0.310, 800.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 4.000, 0.000, 0.000

static_pitch = 0.000
static_cg_height = 10.500


[electrical]
max_battery_voltage = 24.0
generator_alternator_voltage = 28.0
max_generator_alternator_amps = 60.0

[pitot_static]
vertical_speed_time_constant = 1.0              //Increasing this value will cause a more instantaneous reaction in the VSI

[exits]
number_of_exits = 1
exit_rate.0 = 0.4                               ;Percent per second


[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

[Views]
eyepoint = 38.71, -1.4, 5.16   //Longitudinal, Lateral, Vertical (feet)

[LIGHTS]
//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing
light.0 = 3,  -1.60, -62.86,  5.43, fx_navred ,
light.1 = 3,  -1.60,  62.86,  5.43, fx_navgre ,
light.2 = 3, -65.78,   0.00,  6.65, fx_navwhi ,
light.3 = 2,  -1.84, -62.86,  5.43, fx_strobe ,
light.4 = 2,  -1.84,  62.86,  5.43, fx_strobe ,
light.5 = 1,  -8.36,   0.00,  8.77, fx_beacon ,
light.6 = 2,  16.83,   0.00, -2.57, fx_beacon ,
light.7 = 4,  35.58,   0.00,  5.73, fx_vclight,


[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

[fuel]
LeftMain  = 0.000, -10.000, 0.000, 3875.000, 0.000
RightMain = 0.000, 10.000, 0.000, 3875.000, 0.000
fuel_type = 1                                //Fuel type: 1 = Avgas, 2 = JetA
number_of_tank_selectors = 1                    

[EFFECTS]
wake=fx_wake
water=fx_spray
dirt=fx_tchdrt
concrete=fx_sparks
touchdown=fx_tchdwn_s, 1

[airplane_geometry]
wing_area               = 1550.000
wing_span               = 124.000
wing_root_chord         = 18.000
wing_dihedral           = 4.000
wing_incidence          = 0.000
wing_twist              = -1.000
oswald_efficiency_factor= 0.800
wing_winglets_flag      = 0
wing_sweep              = 2.000
wing_pos_apex_lon       = 4.500
wing_pos_apex_vert      = -1.000
htail_area              = 450.000
htail_span              = 50.000
htail_pos_lon           = -60.000
htail_pos_vert          = 7.000
htail_incidence         = 0.000
htail_sweep             = 2.000
vtail_area              = 300.000
vtail_span              = 15.000
vtail_sweep             = 3.000
vtail_pos_lon           = -60.000
vtail_pos_vert          = 10.000
elevator_area           = 120.000
aileron_area            = 100.000
rudder_area             = 120.000
elevator_up_limit       = 17.000
elevator_down_limit     = 15.500
aileron_up_limit        = 18.000
aileron_down_limit      = 18.000
rudder_limit            = 30.000
elevator_trim_limit     = 15.000
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    = 130.000
full_flaps_stall_speed  = 100.000
cruise_speed            = 525.000

[autopilot]
autopilot_available= 1
flight_director_available= 1
default_vertical_speed= 700.0
autothrottle_available= 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

[Flaps.0]
type             =   1
span-outboard    =   0.600
extending-time   =  15.000
system_type      =   1
damaging-speed   = 150.000
blowout-speed    = 250.000
lift_scalar      =   0.500
drag_scalar      =   1.000
pitch_scalar     =   0.500
flaps-position.0 =  00.000, 0.000
flaps-position.1 =  10.000, 0.000
flaps-position.2 =  20.000, 0.000
flaps-position.3 =  30.000, 0.000
flaps-position.4 =  35.000, 0.000