// EC-121 flight dynamics (EC121_FS9.AIR) version 2.3, Wolfram Beckert (Apr 6, 2004)
// for use with Mike Stone's FS2004 Lockheed EC-121 Warning Star (tip tank version) 
// includes a fix for Force Feedback joysticks

// CAUTION!!! Never use FSEDIT for changes of aircraft.cfg. This will spoil many settings in the .AIR file !

[fltsim.0]
title=Lockheed EC-121 Super Warning Star
sim=EC121_FS9
model=
panel=
sound=
texture=
kb_checklists=L1049G_check
kb_reference=L1049G_ref
atc_id=4B
atc_id_enable=1
ui_manufacturer=Lockheed
ui_type=EC-121 Super Warning Star
ui_variation=NAVY
description=Military version of the Super Constellation, equipped with radom and wing-tip fuel tanks.\n\nAircraft design: Mike Stone.\nFS2004 Flight model by Wolfram Beckert.
atc_airline=NAVY
atc_flight_number=502
atc_heavy=0
visual_damage=1

// insert here new [fltsim.N] sections for repaints

[General]
performance=Wingspan:  123 ft. 5 in. (with tip tanks)\nLength:  116 ft. 2 in. (with radar nose fitted)\nHeight:  24 ft. 9.4 in.\nMax takeoff weight:  137,500 lbs.\nMax landing weight:  113,000 lbs.\nPayload:  24,293 lbs.\nMax speed:  318 knots (TAS)\nCruise speed:  270 knots (TAS)\nRange (max fuel):  4184 nm\nRange (max payload):  3619 nm\nService ceiling:  22,800 ft.\nCrew:  5 cockpit, 4 cabin\nPassengers:  75-99\nPower:  4x 3250 bhp Curtiss-Wright R-3350-DA3\nFuel capacity:  6550 gal (7750 gal with tip tanks)
atc_type=LOCKHEED
atc_model=C121
// EC121 does not work
editable=0

[pitot_static]
vertical_speed_time_constant=2.0		//Increasing this value will cause a more instantaneous reaction in the VSI

[WEIGHT_AND_BALANCE]
reference_datum_position= 0.000, 0.000, 0.000
empty_weight_CG_position= 0.000, 0.000, 0.000
max_number_of_stations= 50 
station_load.0= 4800.000, -30.000, 0.000, 0.000, EQ-load rear
station_load.1= 5000.000, 22.000, 0.000, 0.000, EQ-load front
station_load.2= 5000.000, -8.000, 0.000, 0.000, EQ-load center
station_load.3= 800.000, 0.000, 0.000, 0.000, Operator crew
empty_weight= 73356.000
empty_weight_roll_MOI= 2343290.000
empty_weight_pitch_MOI= 4634852.000
empty_weight_yaw_MOI= 3473465.000
empty_weight_coupled_MOI= 0.000
max_gross_weight= 135460.000
CG_forward_limit= 0.000
CG_aft_limit= 0.500 

[flight_tuning]
cruise_lift_scalar=1.000 
pitch_stability=1.000                  
roll_stability=1.000
yaw_stability=1.000
parasite_drag_scalar=1.000    // set about 10 percent more in AIR file as Connie for radome drag
induced_drag_scalar=1.050     // set about 5 percent more as Connie for radome drag
elevator_effectiveness=1.000            
aileron_effectiveness=1.000
rudder_effectiveness=1.100
elevator_trim_effectiveness=1.000      
aileron_trim_effectiveness=1.000
rudder_trim_effectiveness=1.000
p_factor_on_yaw          = 0.5
torque_on_roll           = 1.0
gyro_precession_on_yaw   = 1.0
gyro_precession_on_pitch = 1.0

[flaps.0]
type= 1					// 1 - tail, 2 - lead
span-outboard= 0.700
extending-time= 15.000
system_type= 1
damaging-speed= 210.000
blowout-speed= 230.000
lift_scalar= 1.200
drag_scalar= 1.000
pitch_scalar= 1.000
flaps-position.0= 0.000, 310.000
flaps-position.1= 25.000, 198.000	// KTAS ?
flaps-position.2= 28.000, 178.000
flaps-position.3= 33.600, 165.000
flaps-position.4= 42.000, 155.000

[GeneralEngineData]
engine_type= 0
Engine.0= 4.633, -31.500, -0.417
Engine.1= 5.117, -14.500, -1.533
Engine.2= 5.117, 14.500, -1.533
Engine.3= 4.633, 31.500, -0.417
fuel_flow_scalar= 1.240			// should result in about 630 Gal/h at cruise
min_throttle_limit=0.000000
master_ignition_switch= 0		//Master Ignition Switch
max_contrail_temperature=-20		//choose temp c below which contrails occur 

[piston_engine]
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 
cylinder_displacement= 186.000		// real world 186=3350/18 cuin
compression_ratio= 8.500  
number_of_cylinders= 18
max_rated_rpm= 2900.000
max_rated_hp= 3250.000
fuel_metering_type= 0
cooling_type= 0
normalized_starter_torque= 0.050
turbocharged= 1
max_design_mp= 59.500			// turbocompound chargers and 145 hi-octane fuel
min_design_mp= 5.000
critical_altitude= 11500.000		// limit ceiling alt, not equal to real ceiling !
emergency_boost_type= 0
emergency_boost_mp_offset= 0.000
emergency_boost_gain_offset= 0.000
fuel_air_auto_mixture= 0		// 1 = automix on, 0 = manual mixture set
auto_ignition= 0
power_scalar=1.000

[propeller]
propeller_type= 0
propeller_diameter= 15.150		// real world 15,15 ft
propeller_blades= 3
propeller_moi= 38.500			//  keep rpm above 800, below 900 at idle
beta_max= 45.000 
beta_min= 10.000 
min_gov_rpm= 1000.000			// was 800
prop_tc= 0.004
gear_reduction_ratio= 1.880		//  keep value to fit BMEP
fixed_pitch_beta= 20.000
low_speed_theory_limit= 80.000
prop_sync_available= 1
prop_deice_available= 1
prop_feathering_available= 1
prop_auto_feathering_available= 1
min_rpm_for_feather= 600.000
beta_feather= 83.000
power_absorbed_cf= 0.300
defeathering_accumulators_available= 0
feathering_switches = 1			//Switches which invoke feathering
prop_reverse_available= 0		// prop reverse off
minimum_on_ground_beta= 1.000
minimum_reverse_beta= -25.000
thrust_scalar=1.025                     // was 1.050, fine tune climb and cruise, not real but nice trick


//Gear ans scrape section
        //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

[contact_points]
point.0= 1.000, 39.417, 0.000, -10.403, 1600.000, 0.000, 1.562, 48.000, 0.322, 2.500, 0.573, 5.000, 7.000, 0.000, 165.000, 190.000
point.1= 1.000, -3.383, -14.500, -10.000, 1800.000, 1.000, 2.562, 0.000, 0.383, 2.500, 0.573, 14.000, 17.000, 2.000, 165.000, 190.000
point.2= 1.000, -3.383, 14.500, -10.000, 1800.000, 2.000, 2.562, 0.000, 0.383, 2.500, 0.573, 15.000, 18.000, 3.000, 165.000, 190.000
point.3= 2.000, -7.167, -61.500, 5.500, 874.803, 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, -7.167, 61.500, 5.500, 874.803, 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, -56.417, 0.000, 2.833, 1174.803, 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, 44.417, 0.000, 2.833, 1174.803, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 4.000, 0.000, 0.000

static_pitch= 0.120
static_cg_height= 10.002
gear_system_type=1			// Hydraulic

[gear_warning_system]
gear_warning_available=1
pct_throttle_limit =  0.1		//Percent throttle that activates warning
flap_limit_idle    =  25.0		//Flap angle that activates warning at idle
flap_limit_power   =  33.0		//Flap angle that activates warning at above idle

[brakes]
parking_brake = 1			//Parking brake available
toe_brakes_scale = 0.8			//Brake scalar
differential_braking_scale = 0.5        //Delta on the amount of brake when the rudder pedals deflected

[hydraulic_system]
normal_pressure = 1500.0		//PSI
electric_pumps  = 0			//no electric pumps
engine_map      = 1,1,1,1		//pumps on all Engines

[Views]
eyepoint=34.498, -1.999, 6.101

[LIGHTS]
// these values fit for Mike Stone's model including tip tanks
//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing
light.0 = 3,  -1.70, -62.95,  5.43, fx_navredm
light.1 = 3,  -1.70,  62.95,  5.43, fx_navgrem
light.2 = 3, -65.78,   0.00,  6.65, fx_navwhi
light.3 = 1, -59.81,   0.00, 17.2,  fx_beaconh  // top center fin ec121
light.4 = 1,  16.83,   0.00, -2.58, fx_beaconb
light.5 = 4,  35.58,   0.00,  5.73, fx_vclight
//light.6 = 2,  -1.38, -62.88,  5.43, fx_strobeh		// not available in real aircraft
//light.7 = 2,  -1.38,  62.88,  5.43, fx_strobeh		// not available in real aircraft

[Radios]
// Radio Type=available, standby frequency, has glide slope
Audio.1=1
Com.1=1, 0
Com.2=1, 0
Nav.1=1, 0, 1
Nav.2=1, 0, 1
Adf.1=1
Transponder.1=1
Marker.1=1

[keyboard_response]
elevator=150.000000,190.000000
aileron=150.000000,190.000000
rudder=150.000000,170.000000

[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=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, 1
startup=vncon_engstrt
contrail=fx_Contrail_l			// new automatic contrails at low temperature in FS2k4

[SMOKESYSTEM]
smoke.0=-0.417, 6.333, -31.500, fx_smoke_w
smoke.1=-0.833, 4.917, -14.500, fx_smoke_w
smoke.2=-0.833, 4.917, 14.500, fx_smoke_w
smoke.3=-0.417, 6.333, 31.500, fx_smoke_w

[electrical]
max_battery_voltage=25                  //was 24, shall increase battery lifetime
generator_alternator_voltage=28
max_generator_alternator_amps=100
electric_always_available=0
//			BusType, MaxAmpLoad, MinVoltage
//	BusTypes:0=MainBus,1=AvionicsBus,2=BatteryBus,3=HotBatteryBus,4-7=Generator/AlternatorBus(1-4)   
autopilot=0,  5, 13.0
avionics_bus=0, 10, 13.0
avionics=1,  5, 13.0
pitot_heat=0, 15, 13.0
additional_system=0, 20, 13.0
marker_beacon=1,  2, 13.0
gear_warning=0,  2, 13.0
fuel_pump=0,  5, 13.0
starter1=0, 20, 13.0
starter2=0, 20, 13.0
starter3=0, 20, 13.0
starter4=0, 20, 13.0
light_nav=0,  5, 13.0
light_beacon=0,  5, 13.0
light_landing=0,  5, 13.0
light_taxi=0,  5, 13.0
light_strobe=0,  5, 13.0
light_panel=0,  5, 13.0
light_cabin=0,  5, 13.0
prop_sync=0, 15, 13.0
auto_feather=0, 15, 13.0
propeller_deice=0,  5, 13.0

[fuel]
LeftMain= 0.000, -25.000, 0.000, 1550.000, 0.000
LeftAux= 0.000, -49.167, 0.000, 550.000, 0.000
LeftTip= 2.000, -60.000, 0.000, 600.000, 0.000
RightMain= 0.000, 25.000, 0.000, 1550.000, 0.000
RightAux= 0.000, 49.167, 0.000, 550.000, 0.000
RightTip= 2.000, 60.000, 0.000, 600.000, 0.000
Center1= 5.000, 0.000, 0.000, 1175.000, 0.000
Center2= -15.000, 0.000, 0.000, 1175.000, 0.000
fuel_type=1.000000
number_of_tank_selectors=2
electric_pump=1
//Max. Fuel = 7750 USGal about 29330 Liters, about 46500 lbs

[airplane_geometry]
wing_area= 1650.000
wing_span= 123.000
wing_root_chord= 15.500
wing_dihedral= 7.000
wing_incidence= 2.300			
wing_twist= -1.000
oswald_efficiency_factor= 0.700		
wing_winglets_flag= 0
wing_sweep= 3.000
wing_pos_apex_lon= 3.880
wing_pos_apex_vert= 0.000
htail_area= 500.000                    
htail_span= 49.833
htail_pos_lon= -61.700
htail_pos_vert= 0.000
htail_incidence= -1.900          //was -1.7
htail_sweep= 0.000
vtail_area= 328.000
vtail_span= 20.650
vtail_sweep= 0.000
vtail_pos_lon= -62.500
vtail_pos_vert= 1.500
elevator_area= 215.000                     
aileron_area= 90.000
rudder_area= 114.000
elevator_up_limit= 24.500       //was 27.5
elevator_down_limit= 19.500     //was 24.5
aileron_up_limit= 16.500        //was 19.5
aileron_down_limit= 12.900      //was 14.9
rudder_limit= 25.0
elevator_trim_limit= 19.0       //was20.5
spoiler_limit= 60.0
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= 115.000
full_flaps_stall_speed= 95.000
cruise_speed= 314.000                   // KTAS
max_indicated_speed=280.000000		// Red Line KIAS
max_mach= 0.52

[autopilot]
autopilot_available=1
flight_director_available=0
default_vertical_speed=700		// keep this low to avoid excessive VS when A/P is engaged
autothrottle_available=0		//uncler if real AC had AT
autothrottle_arming_required=0
autothrottle_max_rpm=90
autothrottle_takeoff_ga=0
default_pitch_mode=0			// 0=None, 1=Pitch Hold, 2=Altitude hold
pitch_takeoff_ga=8
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
default_bank_mode=0			// 0=None, 1=Wing Level Hold, 2=Heading Hold
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=1.0			// yaw damper on



[forcefeedback]
// copied from 777 default, btw fully identical to the old Connie tables

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

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