//KC-135T Aircraft.cfg version 1.85, by Rok Dolenec

[fltsim.0]
title=KC135RT Title
sim=KC135RT
model=
panel=
sound=
texture=
kb_checklists=
kb_reference=
atc_id=580045
atc_airline=Air Force
atc_flight_number=0045
atc_heavy=1
ui_manufacturer=Boeing
ui_type=KC-135T
ui_variation=58-0045

description=KC-135 Stratotanker: strategic air refuling station, build by Boeing Company. Can also be used as cargo carier or troop transport.\nVersion 1.85

[General]
atc_type=BOEING AIRCRAFT
atc_model=B717 
performance=Aircraft Basic Weight: 115,000 lb\nMax Takeoff Weight: 297,000 lb\nMaximum Cargo Capability: 75,000 lb, 37 passengers\nPower Plant: Four CFM-56 turbofan engines, 22000 lbs thrust each\s \nWingspan: 130.83 ft \nLength: 136.25 ft\nHeight: 41.67 ft\nSpeed: 530 mph at 30,000 ft\nRange: 1,150 nm with 120,000 lb of transfer fuel\s ferry mission, up to 9,200 nm\n


[pitot_static]
vertical_speed_time_constant = 2                //Increasing this value will cause a more instantaneous reaction in the VSI


[WEIGHT_AND_BALANCE]
max_gross_weight = 297000                       // (pounds)
empty_weight = 115000                           // (pounds)

reference_datum_position     =  0, 0, 0      // (feet) distance from FlightSim Reference position: (1/4 chord, centerline, waterline)
empty_weight_CG_position     =  3, 0, 0      // (feet) longitudinal, lateral, vertical distance from specified datum
//13.84
max_number_of_stations = 5

station_load.0 = 400, 3, 0, 0        //Payload  Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)

;Moments of Inertia
empty_weight_roll_MOI    = 2373514
empty_weight_pitch_MOI   = 2895823
empty_weight_yaw_MOI     = 5173833
empty_weight_coupled_MOI = 0


[fuel]
Center1   =    3.0,   0.0,  0.0, 20348, 28.0    //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)
LeftMain  =    0.0, -10.0,  0.0,  2821, 24.0    //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)
LeftAux   =    0.0, -45.0,  0.0,   434, 1.5     //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)
RightMain =    0.0,  10.0,  0.0,  2821, 24.0    //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)
RightAux  =    0.0,  45.0,  0.0,   434, 1.5     //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)
fuel_type = 2                                   //Fuel type: 1 = Avgas, 2 = JetA
number_of_tank_selectors = 1
//TF:26858 gal = 177263 lbs                
electric_pump=0

[airplane_geometry]//this are for boeing 707-320 but should be close enough
wing_area               = 2941.0                //Square feet
wing_span               = 145.75                //Feet
wing_root_chord         = 20.2//<-MAC, Root->33.5     //Feet
wing_dihedral           = 6.8                   //Degrees
wing_incidence          = 1.0                   //Degrees
wing_twist              = -1.0                  //Degrees
oswald_efficiency_factor= 0.8862                //Measure of lift effeciency of wing
wing_winglets_flag      = 0                     //Are winglets available?
wing_sweep              = 35                    //Degrees, wing leading edge
wing_pos_apex_lon       = 5//22.3                  //Feet, longitudinal distance from reference point, negative going aft
wing_pos_apex_vert      = 0.7                   //Feet, vertical distance from reference point, positive going up
htail_area              = 350                   //Square feet
htail_span              = 42.6                  //Feet
htail_pos_lon           = -60.7                 //Feet, longitudinal distance from reference point, negative going aft
htail_pos_vert          = 7.7                   //Feet, vertical distance from reference point, positive going up
htail_incidence         = 0.0                  //Degrees
htail_sweep             = 35                    //Degrees, horizontal tail leading edge
vtail_area              = 352                   //Square feet
vtail_span              = 24.4                  //Feet, tip to body
vtail_sweep             = 40                    //Degrees, vertical tail leading edge
vtail_pos_lon           = -45.0                 //Feet, longitudinal distance from reference point, negative going aft
vtail_pos_vert          = 11.5                  //Feet, vertical distance from reference point, positive going up
elevator_area           = 200                   //Square feet
aileron_area            = 200                   //Square feet
rudder_area             = 113                   //Square feet
elevator_up_limit       = 30                    //Degrees
elevator_down_limit     = 30                    //Degrees
aileron_up_limit        = 30                    //Degrees
aileron_down_limit      = 20                    //Degrees
rudder_limit            = 35                    //Degrees
elevator_trim_limit     = 30                    //Degrees
spoiler_limit           = 45                    //Degrees
spoilerons_available    = 0                     //Spoilerons Available?
aileron_to_spoileron_gain = 0                   //Aileron to spoileron gain
min_ailerons_for_spoilerons = 0                 //Degrees
min_flaps_for_spoilerons = 0                    //Minimum flap handle position when spoilerons activate

[Reference Speeds]
flaps_up_stall_speed    = 130.0                 //Knots True (KTAS)
full_flaps_stall_speed  = 108.0                 //Knots True (KTAS)
cruise_speed            = 270//<-AI cruise IAS, 527.0                 //Knots True (KTAS)
max_indicated_speed=594.000000
max_mach=0.887012

[flaps.0]
type             = 1                                    // 1 - tail, 2 - lead
span-outboard    = 0.5                                  // 0.0 .. 1.0
extending-time   = 20                                   // seconds
flaps-position.0 = 0                                    // degrees
flaps-position.1 = 20                                   // degrees
flaps-position.2 = 30                                   // degrees
flaps-position.3 = 40                                   // degrees
flaps-position.4 = 50                                   // degrees
damaging-speed   = 250                                  // KIAS
blowout-speed    = 300                                  // KIAS
lift_scalar = 0.6
drag_scalar = 0.7
pitch_scalar= 0.4
system_type = 1                                         //Hydraulic

[flaps.1]
type             = 2                                    // 1 - tail, 2 - lead
span-outboard    = 0.3                                  // 0.0 .. 1.0
extending-time   = 10                                   // seconds
flaps-position.0 = 0                                    // degrees
flaps-position.1 = 20                                   // degrees
flaps-position.2 = 30                                   // degrees
flaps-position.3 = 40                                   // degrees
flaps-position.4 = 50                                   // degrees                                  // degrees
damaging-speed   = 250                                  // KIAS
blowout-speed    = 300                                  // KIAS
lift_scalar = 0.6
drag_scalar = 0.7
pitch_scalar= 0.4
system_type = 1                                         //Hydraulic

[flight_tuning]
cruise_lift_scalar     = 0.9
parasite_drag_scalar   = 1.0
induced_drag_scalar    = 1.0
elevator_effectiveness = 1.0
aileron_effectiveness  = 1.0
rudder_effectiveness   = 1.3
pitch_stability        = 0.9
roll_stability         = 1.0
yaw_stability          = 1.0
elevator_trim_effectiveness = 0.25
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 = -15.36, -46.30,  0.36                //(feet) longitudinal, lateral, vertical distance from reference datum
Engine.1 =   0.00, -27.05, -2.19                //(feet) longitudinal, lateral, vertical distance from reference datum
Engine.2 =   0.00,  27.05, -2.19                //(feet) longitudinal, lateral, vertical distance from reference datum
Engine.3 = -15.36,  46.30,  0.36                //(feet) longitudinal, lateral, vertical distance from reference datum
fuel_flow_scalar        = 1.0                   //Scalar for fuel flow efficiency
min_throttle_limit= 0

[TurbineEngineData]
fuel_flow_gain          = 0.002                 //Gain on fuel flow
inlet_area              = 12                  //Square Feet, engine nacelle inlet area
rated_N2_rpm            = 29920                 //RPM, second stage compressor rated value
static_thrust           = 21643                 //Lbs, max rated static thrust at Sea Level
afterburner_available   = 0                     //Afterburner available?
reverser_available      = 0                     //Thrust reverser available?

[jet_engine]
thrust_scalar = 1.0

[autopilot]
autopilot_available             = 1
flight_director_available       = 1
default_vertical_speed          = 1800
autothrottle_available          = 1
autothrottle_arming_required    = 1
autothrottle_max_rpm            = 90
autothrottle_takeoff_ga         = 1
pitch_takeoff_ga                = 8;
max_pitch=10.000000
max_pitch_acceleration=1.000000
max_pitch_velocity_lo_alt=2.000000
max_pitch_velocity_hi_alt=1.500000
max_pitch_velocity_lo_alt_breakpoint=20000.000000
max_pitch_velocity_hi_alt_breakpoint=28000.000000
max_bank=25.000000
max_bank_acceleration=1.800000
max_bank_velocity=3.000000
max_throttle_rate=0.100000
nav_proportional_control=9.000000
nav_integrator_control=0.250000
nav_derivative_control=0.000000
nav_integrator_boundary=2.500000
nav_derivative_boundary=0.000000
gs_proportional_control=9.520000
gs_integrator_control=0.260000
gs_derivative_control=0.000000
gs_integrator_boundary=0.700000
gs_derivative_boundary=0.000000
yaw_damper_gain=0.000000

[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= 1.000, 42.600, 0.000, -7.970, 1575.000, 0.000, 1.530, 70.000, 0.391, 2.500, 0.900, 5.500, 5.500, 0.000, 0.000, 0.000
point.1= 1.000, -0.940, -8.730, -7.970, 2000.000, 1.000, 1.870, 0.000, 0.391, 2.500, 0.567, 6.800, 9.800, 2.000, 0.000, 0.000
point.2= 1.000, -0.940, 8.730, -7.970, 2000.000, 2.000, 1.870, 0.000, 0.391, 2.500, 0.567, 10.200, 10.200, 3.000, 0.000, 0.000
point.3= 2.000, -24.600, -66.300, 7.550, 787.400, 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, -24.600, 66.300, 7.550, 787.400, 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, -65.600, 0.000, 6.560, 787.400, 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, 37.100, 0.000, -3.281, 787.400, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 4.000, 0.000, 0.000

static_pitch = 0.0
static_cg_height = 7.97
gear_system_type=1

[Views]
eyepoint= 56.75, -1.80, 7.95              ; Longitude, Latitude and Vertical position from Reference Point, (FEET)

[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, 10, 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_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

[hydraulic_system]
electric_pumps=0
engine_map=1,1,1,1
//normal_pressure=3680
normal_pressure=3000

[Radios]
// Radio Type = availiable, 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, 0
Adf.1         = 1
Transponder.1 = 1
Marker.1      = 1

[LIGHTS]
//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing                   
light.0 = 3, -27.65,  66.20,  7.71, fx_navgreh ,//right wing nav green
light.1 = 3, -27.65, -66.20,  7.71, fx_navredh ,//left wing nav red
light.2 = 2, -27.65,  66.20,  7.71, fx_strobeh ,//right strobe white
light.3 = 2, -27.65, -66.20,  7.71, fx_strobeh ,//left strobe white
light.4 = 2, -68.94,  -0.01,  9.76, fx_beaconb ,//tail strobe red
light.5 = 2, -68.94,  -0.01,  9.41, fx_strobeh ,//tail strobe white
light.6 = 2,   0.00,   0.00, -3.56, fx_beaconb ,//lower beacon
light.7 = 2,   0.00,   0.00, 11.65, fx_beaconb ,//upper beacon
light.8 = 4, 55.00,   0.00,  7.80, fx_vclighth ,//virtual cockpit
light.9 = 4, 27.00,   0.00,  7.00, fx_vclighth ,//Cargo hold

[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

[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 = 350, 500
aileron  = 450, 1000
rudder   = 200, 1000

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

[exits]
number_of_exits = 2
exit_rate.0 = 0.4                               ;Percent per second
exit_rate.1 = 0.4                               ;Percent per second

[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
[brakes]
toe_brakes_scale=0.640889
parking_brake=1
[gear_warning_system]
gear_warning_available=1
pct_throttle_limit=0.099976
flap_limit_power=25.496622
flap_limit_idle=5.042029
[stall_warning]
type=1
[attitude_indicators]
attitude_indicator.0=1
[turn_indicators]
turn_indicator.0=1,0