[fltsim.0]
title=KC-135R Stratotanker
sim=KC135R
model=
panel=
sound=
texture=
kb_checklists=
kb_reference=
atc_id=N700MS
atc_airline=Air Force
atc_flight_number=1123
atc_heavy=1
ui_manufacturer=Boeing
ui_type=KC-135R
ui_variation=
description=KC-135R Stratotanker: strategic air refuling station, build by Boeing Company. Can also be used as cargo carier or troop transport.

[General]
atc_type=BOEING AIRCRAFT
atc_model=B703
performance=Aircraft Basic Weight: 123,000 lb\nMax Takeoff Weight: 323,000 lb\nMaximum Cargo Capability: 83,000 lb, 37 passengers\nPower Plant: Four CFM-56 turbofan engines, 21,634 lb thrust each\s \nWingspan: 130.83 ft\nLength: 136.25 ft\nHeight: 41.67 ft\nSpeed: 530 mph per hour at 30,000 ft\nCeiling: 50,000 ft\nRange: 1,500 nm with 150,000 lb of transfer fuel\s ferry mission, up to 11,000 nm\n

[WEIGHT_AND_BALANCE]
max_gross_weight= 323000.000
empty_weight= 123000.000

reference_datum_position= 0.000, 0.000, 0.000
empty_weight_CG_position= 6.000, 0.000, 0.000

max_number_of_stations= 50

station_load.0= 74957.000, 6.000, 0.000, 0.000

;Moments of Inertia
empty_weight_pitch_MOI= 25000000.000
empty_weight_roll_MOI= 2600000.000
empty_weight_yaw_MOI= 4500000.000
empty_weight_coupled_MOI= 0.000
CG_forward_limit= 0.000
CG_aft_limit= 1.000

[flight_tuning]
cruise_lift_scalar=0.505
parasite_drag_scalar=0.582
induced_drag_scalar=0.920
elevator_effectiveness=1.000
aileron_effectiveness=1.121
rudder_effectiveness=1.500
pitch_stability=1.000
roll_stability=1.000
yaw_stability=1.000
elevator_trim_effectiveness=0.910
aileron_trim_effectiveness=1.000
rudder_trim_effectiveness=1.000

[GeneralEngineData]
engine_type= 1
Engine.0= -8.957, -46.320, 0.848
Engine.1= 5.971, -27.120, -0.976
fuel_flow_scalar= 1.100
Engine.2= 5.971, 27.120, -0.976
Engine.3= -8.957, 46.320, 0.848

[TurbineEngineData]
fuel_flow_gain= 0.002
inlet_area= 27.850
rated_N2_rpm= 29920.000
static_thrust= 21634.000
afterburner_available= 0
reverser_available= 1

[jet_engine]
thrust_scalar=1.000

[electrical]
;BusType, MaxAmpLoad, MinVoltage       BusTypes:0=MainBus,1=AvionicsBus,2=BatteryBus,3=HotBatteryBus,4-7=Generator/AlternatorBus(1-4)
flap_motor=0, 5 , 17.0
gear_motor=0, 5 , 17.0
autopilot=0, 5 , 17.0
avionics_bus=0, 10, 17.0
avionics=1, 5 , 17.0
pitot_heat=0, 2 , 17.0
additional_system=0, 20, 17.0
marker_beacon=1, 2 , 17.0
gear_warning=0, 2 , 17.0
fuel_pump=0, 5 , 17.0
starter1=0, 20, 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

//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= 1.000, 42.600, 0.000, -7.970, 1575.000, 0.000, 1.530, 70.000, 0.391, 2.500, 0.900, 4.000, 4.000, 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, 6.900, 6.900, 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, 7.100, 7.100, 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= 0.000
static_cg_height= 7.990

[Views]
eyepoint= 56.75, -1.80, 7.95

[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

[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

[LIGHTS]       
//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing
light.0=3, -26.87,  66.10,  7.46, fx_navgrem ,
light.1=3, -26.87, -66.10,  7.46, fx_navredm ,
light.2=2, -26.00, -66.10,  7.46, fx_strobeh ,
light.3=2, -26.00,  66.10,  7.46, fx_strobeh ,
light.4=2, -68.90,   0.00,  9.06, fx_strobeh ,
light.5=1,   0.00,   0.00, -3.56, fx_beaconb ,
light.6=3,  34.00,  -1.74, -3.20, fx_navwhi ,
light.7=3,  34.00,   1.74, -3.20, fx_navwhi ,
light.8=3,  30.33,  -1.74, -3.20, fx_navwhi ,
light.9=3,  30.33,   1.74, -3.20, fx_navwhi ,
light.10=3, 26.67,  -1.74, -3.20, fx_navwhi ,
light.11=3, 26.67,   1.74, -3.20, fx_navwhi ,
light.12=3, 23.00,  -1.74, -3.20, fx_navwhi ,
light.13=3, 23.00,   1.74, -3.20, fx_navwhi ,
light.14=4, 55.00,   0.00,  7.80, fx_vclighth ,

[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

[fuel]
Center1= 0.000, 0.000, 0.000, 4650.000, 0.000
LeftMain= 0.000, -30.000, 0.000, 7000.000, 0.000
RightMain= 0.000, 30.000, 0.000, 7000.000, 0.000
fuel_type=2                                   //Fuel type: 1 = Avgas, 2 = JetA
number_of_tank_selectors=1
                   

[airplane_geometry]
wing_area= 3689.000
wing_span= 130.000
wing_root_chord= 23.000
wing_dihedral= 6.800
wing_incidence= 0.000
wing_twist= -0.500
oswald_efficiency_factor= 0.760
wing_winglets_flag= 0
wing_sweep= 35.000
wing_pos_apex_lon= 25.000
wing_pos_apex_vert= 0.000
htail_area= 988.000
htail_span= 42.000
htail_pos_lon= -100.000
htail_pos_vert= 0.000
htail_incidence= 0.000
htail_sweep= 35.000
vtail_area= 507.000
vtail_span= 27.000
vtail_sweep= 40.000
vtail_pos_lon= -108.000
vtail_pos_vert= 5.800
elevator_area= 154.000
aileron_area= 223.000
rudder_area= 111.000
elevator_up_limit= 30.000
elevator_down_limit= 30.000
aileron_up_limit= 30.000
aileron_down_limit= 20.000
rudder_limit= 30.000
elevator_trim_limit= 30.000
spoiler_limit= 45.000
spoilerons_available= 1
aileron_to_spoileron_gain= 3.000
min_ailerons_for_spoilerons= 10.000
min_flaps_for_spoilerons= 0.000

[Reference Speeds]
flaps_up_stall_speed= 130.000
full_flaps_stall_speed= 108.000
cruise_speed= 530.000

[autopilot]
autopilot_available=1
flight_director_available=1
default_vertical_speed=1800.0
autothrottle_available=1
autothrottle_arming_required=1
autothrottle_max_rpm=90
autothrottle_takeoff_ga=1
pitch_takeoff_ga=8;


[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= 2
span-outboard= 0.800
extending-time= 10.000
system_type= 0
damaging-speed= 0.000
blowout-speed= 0.000
lift_scalar= 1.400
drag_scalar= 0.250
pitch_scalar= 0.500
flaps-position.0= 0.000, 0.000
flaps-position.1= 5.000, 0.000
flaps-position.2= 10.000, 0.000
flaps-position.3= 15.000, 0.000
flaps-position.4= 20.000, 0.000
flaps-position.5= 25.000, 0.000
flaps-position.6= 30.000, 0.000
flaps-position.7= 35.000, 0.000
flaps-position.8= 40.000, 0.000
[Flaps.1]
type= 1
span-outboard= 0.500
extending-time= 20.000
system_type= 0
damaging-speed= 0.000
blowout-speed= 0.000
lift_scalar= 1.500
drag_scalar= 0.250
pitch_scalar= 0.500
flaps-position.0= 0.000, 0.000
flaps-position.1= 5.000, 0.000
flaps-position.2= 10.000, 0.000
flaps-position.3= 15.000, 0.000
flaps-position.4= 20.000, 0.000
flaps-position.5= 25.000, 0.000
flaps-position.6= 30.000, 0.000
flaps-position.7= 35.000, 0.000
flaps-position.8= 40.000, 0.000