[fltsim.0]
title=X-47B DXT3
sim=X-47BFinal
model=
panel=2
sound=
texture=DXT3
kb_checklists=

atc_id=
ui_manufacturer=Northrop Grumman
ui_type=X-47B UCAS D
ui_variation=Navy 501 Demonstrator
atc_flight_number=501
description=Northrop Grumman X-47B Demonstrator\n\nThe X-47B was designed to be adept at long-range surveillance because of its large range and high flight ceiling. Much more than an ordinary drone aircraft the X-47B will be a beast. It has a 62-ft wingspan and weigh around 45,000 pounds at takeoff. The X-47B is designed for stealth. This aircraft shows the Navy's growing embrace of unmanned technology.The X-47B would be a technological step forward having the ability to execute some maneuvers, such as refueling in midflight, autonomously.

[General]
atc_type=NAVY
atc_model=X-47B
editable=0
performance=Model: Andre Thomas\nFlight Dynamics: Andre Thomas\nPaint: Andre Thomas\n\nPhysical Aircraft Characteristics\n\nLenth: 38.2 ft\nWingspan: 62.1 ft\nHeight: 10.4 ft\nMax Takeoff Weight: 44,567 lbs\nPerformance\n\nPower PLant: 1 x Pratt & Whitney F100-220 turbofan\nTrust: 17,800 lbs\nMaximum Speed: "High Subsonic"\nCuise Speed: "High Subsonic"\nRange: 2,100+ Nautical Miles\nService Ceiling: 40,000 ft\n\nArmament/Ordinance: 2 x JDAM (905 kg each); Sensors: EO/IR/SAR/GMTI/ESM/IO


[Views]
eyepoint=17.00, -1.80,  2.70



[Reference Speeds]
flaps_up_stall_speed=	125.00 
full_flaps_stall_speed=	135.00 
cruise_speed=		450.00 
max_indicated_speed=	650.00
max_mach=		  0.95


[weight_and_balance]
max_gross_weight = 	44567
empty_weight = 		14000

reference_datum_position = 	0.00, 0.00, 0.00
empty_weight_CG_position = 	0.00, 0.00, 0.00
CG_forward_limit = 		      0.19
CG_aft_limit =   		      0.29

empty_weight_pitch_MOI = 	  78000.00
empty_weight_roll_MOI =  	  47000.00
empty_weight_yaw_MOI= 		  75000.00
empty_weight_coupled_MOI = 	      0.00

max_number_of_stations = 11

station_load.0 =  205.00, 0.00, 0.00, 0.00,  Pilot
station_load.1 =  210.00, 0.00, 0.00, 0.00,  Navigator
station_load.2 =  225.00, 0.00, 0.00, 0.00,  ECM Op.
station_load.3 =  195.00, 0.00, 0.00, 0.00,  ECM Op.2
station_load.4 =  200.00, 0.00, 0.00, 0.00,  Survival Gear
station_load.5 =    0.00,-3.00,-8.00,-3.50,  Left Drop Tank
station_load.6 =    0.00,-3.00, 8.00,-3.50,  Right Drop Tank
station_load.7 =    0.00, 0.00, 0.00, 0.00,  5x AN/ALQ-99
station_load.8 =    0.00, 0.00, 0.00, 0.00,  3x AN/ALQ-99
station_load.9 =    0.00, 0.00, 0.00, 0.00,  2x AGM88 HARM
station_load.10=    0.00, 0.00, 0.00, 0.00,  4x AGM88 HARM



[lights]
//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing

light.0 = 9,    3.10,    0.00,   1.25, fx_Alpha_EA6_vapour1, //Low Speed
light.1 = 7,  -11.31,-30.86, -1.00, fx_Alpha_EA6_Vortices, //Wingtip
light.2 = 7,  -11.31, 30.86, -1.00, fx_Alpha_EA6_Vortices, //Wingtip

light.3 = 1,  -10.00,  -26.75,   0.80, fx_Alpha_EA6_Vortices1, //Flaps
light.4 = 1,  -10.00,   26.75,   0.80, fx_Alpha_EA6_Vortices1, //Flaps


light.5= 8,   3.10,    0.00,   1.25, fx_Alpha_EA6_vapour1, //Wingfence


light.6  = 7, -10.00,  0.00,  0.00,fx_nicksmokeAI_777_AB
light.7  = 3, -11.31,-30.86, -1.00,fx_navredm //Navigation Red (Left Wing)
light.8  = 3, -11.31, 30.86, -1.00,fx_navgrem //Navigation Green (Right Wing)
light.9  = 2, -11.31,-30.86, -1.00,fx_strobeh //Strobe White (Left Wing)
light.10 = 2, -11.31, 30.86, -1.00,fx_strobeh //strobe White (Right Wing)

light.12 = 3,  -2.58,  0.00, -3.46,fx_beaconh //Beacon Bottom
light.13 = 3,   6.58,  0.00,  3.26,fx_beaconh //Beacon Top



[effects]
dirt = 					fx_tchdrt
concrete = 				fx_sparks
touchdown = 				fx_Alpha_EA6_td
windshield_rain_effect_available = 	1


[fuel]
fuel_type = 	           2
number_of_tank_selectors = 1
electric_pump =            1

Center1 =     1.20,   0.00,  2.00,  1000.00,  0.00
leftmain=    -0.20, -10.00,  1.00,   690.00,  0.00
rightmain=   -0.20,  10.00,  1.00,   690.00,  0.00
external1=   -3.00,  -8.00, -3.50,   300.00,  0.00	//Left inboard drop tank
external2 =  -3.00,   8.00, -3.50,   300.00,  0.00	//Right inboard drop tank




[GeneralEngineData]
engine_type=1
Engine.0=0.000000,0.000000,0.000000 
fuel_flow_scalar=1.000000
min_throttle_limit=-0.1
max_contrail_temperature=-60


[TurbineEngineData]
fuel_flow_gain= 0.01 		//Gain on fuel flow
inlet_area= 11.000 		//Square Feet, engine nacelle inlet area
rated_N2_rpm= 29920.000 	//RPM, second stage compressor rated value
static_thrust= 23450.000 	//Lbs, max rated static thrust at Sea Level
afterburner_available= 0 	//Afterburner available?
reverser_available= 0.0  	//Thrust reverser available?

[Jet_Engine]
thrust_scalar=1.0 



[contact_points]
  
        //0  Class			  (1= landing gear/2= scrape point/3= skid point /4= float/5= water rudder)
        //1  Longitudinal Position        (feet from reference datum)
        //2  Lateral Position             (feet from reference datum, minus=Left, plus=Right )
        //3  Vertical Position            (feet from reference datum)
        //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 (max compression/static compression)
        //10 Damping Ratio                (0=Undamped, 1=Critically Damped)
        //11 Extension Time               (seconds)
        //12 Retraction Time              (seconds)
        //13 Sound Type			  (0=Center gear/1=Auxiliary gear/2=Left gear/3=Right gear/4=Fuselage scrape
					   5=Left wing scrape/6=Right wing scrape/7=Aux. scrape 1/8=Aux. Scrape 2/9= Tail scrape)
	//14 IAS limit gear retraction    (KIAS)
        //15 IAS gear damage at 	  (KIAS)
	//Nosewheel travel, this model:	  0.915ft
	//Main gear travel, this model:	  0.892ft


max_number_of_points = 10


//--------0-----1-------2-------3--------4------5-----6-------7-----8------9------10-----11-----12----13---14---15-


//-Gear  0    1      2     3        4       5     6          7         8         9         10      11   12   13   14   15
point.0= 1, 14.67, 0.70,-7.58, 1574.803150, 0, 0.860594, 44.400000, 1.411626, 1.500000, 0.765282, 5.00,5.00,0.00,0.00,0.00

point.1= 1, 14.67,-0.70,-7.58, 1574.803150, 0, 0.860594, 44.400000, 1.411626, 1.500000, 0.765282, 5.00,5.00,0.00,0.00,0.00

point.2= 1, -3.47, 7.50,-7.78, 1574.803150, 2, 0.860594, 0.000000,  1.661853, 1.800000, 0.385852, 5.00,5.00,3.00,0.00,0.00

point.3= 1, -3.47,-7.50,-7.78, 1574.803150, 1, 0.860594, 0.000000,  1.661853, 1.800000, 0.385852, 5.00,5.00,3.00,0.00,0.00


//---- Aircraft Scrape Points
//Left Wing
point.4= 2,-11.31,-30.86, -1.00, 1574.803150, 0,    0.00 ,  0.00   ,      0.00,     0.00,     0.00, 0.00,0.00,6.00,0.00,0.00
  
//Right Wing
point.5= 2,-11.31, 30.86, -1.00, 1574.803150, 0,    0.00,   0.00   ,      0.00,     0.00,     0.00, 0.00,0.00,6.00,0.00,0.00

point.6= 2, -9.58,  0.00,-6.66,1574.803150, 0,    0.00,   0.00   ,      0.00,     0.00,     0.00, 0.00,0.00,9.00,0.00,0.00

point.7= 2, 17.50,  0.00,-6.66,1574.803150, 0,    0.00,   0.00   ,      0.00,     0.00,     0.00, 0.00,0.00,4.00,0.00,0.00

static_pitch=0.000000
static_cg_height=7.853791
gear_system_type=0
gear_system_type = 1



[brakes]
parking_brake=		     1
toe_brakes_scale=	     0.70
differential_braking_scale = 0.20



[hydraulic_system]
electric_pumps= 1
engine_map=	1,1
normal_pressure=3000.00



[flight_tuning]
cruise_lift_scalar=		  1.00 
pitch_stability=  		  1.00 
roll_stability=			  1.00 
yaw_stability=			  1.00
parasite_drag_scalar=		  1.00 
induced_drag_scalar=		  1.00 
elevator_effectiveness=		  1.00 
aileron_effectiveness=		  1.00 
rudder_effectiveness=		  1.00 
elevator_trim_effectiveness=	  1.00 
aileron_trim_effectiveness=	  1.00 
rudder_trim_effectiveness=	  1.00 



[airplane_geometry]
wing_area =			529.00
wing_span = 			 53.00
wing_root_chord = 		 15.00
wing_dihedral = 		  0.00
wing_incidence = 		  0.00
wing_twist = 			  0.00
oswald_efficiency_factor = 	  0.85
wing_winglets_flag = 		  0
wing_sweep = 			 26.00
wing_pos_apex_lon = 		  7.80
wing_pos_apex_vert = 		  0.00
htail_area = 			108.56
htail_span = 			 20.50
htail_pos_lon = 	        -21.00
htail_pos_vert = 		 10.00
htail_incidence = 		  1.00
htail_sweep = 			 30.00
vtail_area = 			 35.04
vtail_span = 			  7.40
vtail_sweep = 			 38.00
vtail_pos_lon =      		-19.50
vtail_pos_vert = 		  3.90
elevator_area = 		 54.28
aileron_area = 			 49.28
rudder_area = 			 17.52
elevator_up_limit = 		 20.00
elevator_down_limit = 		 15.00
aileron_up_limit = 		 51.00
aileron_down_limit = 		 51.00
rudder_limit = 			 35.00
elevator_trim_limit = 		 12.00
spoiler_limit = 		 60.00
aileron_to_spoileron_gain =       0.00
spoiler_handle_available =        1
min_ailerons_for_spoilerons =     0.00
min_flaps_for_spoilerons =        0.00
spoilerons_available = 		  0
spoiler_extension_time=		  0.75
positive_g_limit_flaps_up=	  6.50
positive_g_limit_flaps_down=	  5.00
negative_g_limit_flaps_up=	 -2.40
negative_g_limit_flaps_down=	 -2.00



[Flaps.0]
type= 		    1		
span-outboard=      0.50
extending-time=     5.00
system_type=        0
damaging-speed=   270.00
blowout-speed=    280.00
lift_scalar=        0.35
drag_scalar=        0.75
pitch_scalar=       1.00
flaps-position.0=   0.00,    0.00
flaps-position.1=  75.00,  180.00
flaps-position.2= 100.00,  140.00


[Flaps.1]
type= 		    2
span-outboard=      0.50
extending-time=     5.00
system_type=        0
damaging-speed=   270.00
blowout-speed=    280.00
lift_scalar=        0.50
drag_scalar=        0.12
pitch_scalar=       0.00
flaps-position.0=   0.00,    0.00
flaps-position.1= 100.00,  250.00
flaps-position.2= 100.00,  250.00




[keyboard_response]
elevator = 150.00, 250.00
aileron =  150.00, 150.00
rudder =   150.00, 250.00



[forcefeedback]
gear_bump_nose_magnitude = 	1000
gear_bump_nose_direction = 	18000
gear_bump_nose_duration = 	250000
gear_bump_left_magnitude = 	2000
gear_bump_left_direction = 	35500
gear_bump_left_duration = 	250000
gear_bump_right_magnitude = 	2000
gear_bump_right_direction = 	500
gear_bump_right_duration = 	250000
ground_bumps_magnitude1 = 	1250
ground_bumps_angle1 = 		8900
ground_bumps_intercept1 = 	5
ground_bumps_slope1 = 		0.48
ground_bumps_magnitude2 = 	450
ground_bumps_angle2 =		9100
ground_bumps_intercept2 = 	0.075
ground_bumps_slope2 = 		1
crash_magnitude1 = 		2000
crash_direction1 = 		1000
crash_magnitude2 = 		2000
crash_direction2 = 		9000
crash_period2 = 		7500
crash_duration2 = 		2500000
stick_shaker_magnitude = 	2000
stick_shaker_direction = 	0
stick_shaker_period = 		111111




[electrical]
max_battery_voltage = 		24
generator_alternator_voltage =  28
max_generator_alternator_amps = 65
engine_generator_map = 		1,1
electric_always_available = 	1

flap_motor = 			2,  5,  0
gear_motor = 			2,  5,  0
autopilot = 			1,  5,  0
avionics_bus = 			2, 10,  0
avionics = 			1,  5,  0
pitot_heat = 			2,  2,  0
additional_system = 		2, 20,  0
marker_beacon = 		2,  2,  0
gear_warning = 			2,  2,  0
fuel_pump = 			2,  5,  0
starter1 = 			2, 20,  0
starter2 = 			2, 20,  0
light_nav = 			2,  5,  0
light_beacon = 			2,  5,  0
light_landing = 		2,  5,  0 
light_taxi = 			2,  5,  0
light_strobe = 			2,  5,  0
light_panel = 			2,  5,  0
standby_vacuum = 		2, 15, 17
hydraulic_pump = 		2,  2, 17
fuel_transfer_pump = 		2,  5, 17
light_recognition = 		2,  5, 17
light_wing = 			2,  5, 17
light_logo = 			2,  5, 17
light_cabin = 			2,  0,  0
directional_gyro = 		2,  0,  0
directional_gyro_slaving = 	2,  0,  0



[autopilot]
autopilot_available=		1 
flight_director_available=	1 
default_vertical_speed=	      100.00
default_pitch_mode= 		0
default_bank_mode= 		0 
autothrottle_available=		1 
autothrottle_arming_required=	0
autothrottle_takeoff_ga=	0
autothrottle_max_rpm=		99.00
pitch_takeoff_ga=		15.00
max_pitch=			10.00
max_pitch_acceleration=		1.00
max_pitch_velocity_lo_alt=	2.50
max_pitch_velocity_hi_alt=	0.35
max_pitch_velocity_lo_alt_breakpoint=10000.00
max_pitch_velocity_hi_alt_breakpoint=18000.00
max_bank=		       30.00
max_bank_acceleration=		3.50
max_bank_velocity=		3.50
max_throttle_rate=	        0.10
nav_proportional_control=      20.00
nav_integrator_control=		0.25
nav_derivative_control=		0.00
nav_integrator_boundary=	2.50
nav_derivative_boundary=	0.00
gs_proportional_control=       27.00
gs_integrator_control=	        0.26
gs_derivative_control=		0.00
gs_integrator_boundary=		0.70
gs_derivative_boundary=	        0.00
yaw_damper_gain=		1.00



[Radios]
Audio.1=1 
Com.1=1,0 
Com.2=1,0 
Nav.1=1,0,1 
Nav.2=1,0,0 
Adf.1=1,0 
Transponder.1=1 
Marker.1=1 



[TailHook]
tailhook_length   =   4.05
tailhook_position = -17.00, 0.00, -1.3
cable_force_adjust =  1.00



[folding_wings]
wing_fold_system_type = 4			;0=None
fold_rates = 0.10,0.10				;Percent per second
  


[stall_warning]
type=1



[attitude_indicators]
attitude_indicator.0=1



[turn_indicators]
turn_indicator.0=1,0



[direction_indicators]
direction_indicator.0=3,0 



[stall_warning]
type=1
stick_shaker=0



[GPWS] 
max_warning_height         =  0 
sink_rate_fpm              = -9999 
excessive_sink_rate_fpm    = -9999 
climbout_sink_rate_fpm     = -9999 
flap_and_gear_sink_rate_fpm= -9999



[exits]
number_of_exits=2
exit_rate.0=0.5
exit_rate.1=0.5



[pitot_static]
pitot_heat=1.00



[deice_system]
structural_deice_type=0



[pneumatic_system]
max_pressure=		18.00
bleed_air_scalar=	 0.15



[vacuum_system]
max_pressure=		 5.15
vacuum_type=		 1
electric_backup_pressure=4.90
engine_map=		 1,1



[gear_warning_system]
gear_warning_available=	0
pct_throttle_limit=	0.00
flap_limit_power=	0.00
flap_limit_idle=	0.00