--mounting 3d model paths and texture paths 

mount_vfs_model_path (current_mod_path.."/Shapes")
mount_vfs_liveries_path (current_mod_path.."/Liveries")
mount_vfs_texture_path  (current_mod_path.."/Textures/Bayraktar_TB2_UAV.zip")
mount_vfs_texture_path  (current_mod_path.."/Textures")
--mount_vfs_texture_path  (current_mod_path.."/Textures/Avionics")
--mount_vfs_texture_path  (current_mod_path.."/Textures")
--mount_vfs_texture_path  (current_mod_path.."/Textures/Textures_Cockpit_MQ9_PREDATOR_B.zip")


Bayraktar_TB2_UAV =  {
        
	Name 				=   'Bayraktar_TB2_UAV',
	DisplayName			= _('Bayraktar_TB2_UAV'),
	Cannon 				= "yes",
	HumanCockpit 		= true,
	HumanCockpitPath    = current_mod_path..'/Cockpit/',--current_mod_path..'/Cockpit/
	Picture 			= "MQ9_PREDATOR_B.png",
	Rate 				= 40, -- RewardPoint in Multiplayer
	Shape 				= "Bayraktar_TB2_UAV",
	WorldID             = WSTYPE_PLACEHOLDER,
	shape_table_data 	= 
	{
		{
			file  	 	= 'Bayraktar_TB2_UAV';
			life  	 	= 20; -- lifebar
			vis   	 	= 3; -- visibility gain.
			desrt    		= 'Predator-oblomok'; -- Name of destroyed object file name
			fire  	 	= { 300, 2}; -- Fire on the ground after destoyed: 300sec 2m
			username	= 'Bayraktar_TB2_UAV';
			index    	=  WSTYPE_PLACEHOLDER;
			classname 	= "lLandPlane";
			positioning = "BYNORMAL";
			drawonmap 	= true;
		},
		{
			name  = "MQ9_PREDATOR-oblomok";
			file  = "MQ9_PREDATOR-oblomok";
			fire  = { 240, 2};
		},

	},
	mapclasskey 		= "P0091000024",
	attribute  			= {wsType_Air, wsType_Airplane, wsType_Fighter, WSTYPE_PLACEHOLDER ,"Battleplanes","UAVs",},
	Categories= {"{78EFB7A2-FD52-4b57-A6A6-3BF0E1D6555F}", "",},	
	-------------------------	
		M_empty 					= 1600, -- kg
	M_nominal 					= 3500, -- kg
	M_max 						= 4450, -- kg
	M_fuel_max 					= 1500, -- kg --2225
	H_max 					 	= 13000, -- m
	average_fuel_consumption 	= 0.302, -- this is highly relative, but good estimates are 36-40l/min = 28-31kg/min = 0.47-0.52kg/s -- 45l/min = 35kg/min = 0.583kg/s
	CAS_min 					= 56, -- if this is not OVERAL FLIGHT TIME, but jus LOITER TIME, than it sholud be 10-15 minutes.....CAS capability in minute (for AI)
	V_opt 						= 125,-- Cruise speed (for AI)
	V_take_off 					= 53, -- Take off speed in m/s (for AI)
	V_land 						= 50, -- Land speed in m/s (for AI)
	V_max_sea_level 			= 208, -- Max speed at sea level in m/s (for AI)
	V_max_h 					= 230, -- Max speed at max altitude in m/s (for AI)
	Vy_max 						= 22, -- Max climb speed in m/s (for AI)
	Mach_max 					= 0.76, -- Max speed in Mach (for AI)
	Ny_min 						= -4, -- Min G (for AI)
	Ny_max 						= 8.0,  -- Max G (for AI)
	Ny_max_e 					= 8.0,  -- Max G (for AI)
	AOA_take_off 				= 0.157, -- AoA in take off (for AI)
	bank_angle_max 				= 60, -- Max bank angle (for AI)
		has_afteburner	=	false,
		has_speedbrake	=	false,
		nose_gear_pos				= 	{3.769,	-1.790,	0}, -- nosegear coord 3.769,	-2.353,	0
	    main_gear_pos  				= 	{-0.11,	-2.10,	1.187},
		nose_gear_amortizer_direct_stroke    =  1.795 - 1.795,  -- down from nose_gear_pos !!!
		nose_gear_amortizer_reversal_stroke  =  1.695 - 1.795,  -- up 
		main_gear_amortizer_direct_stroke	 =  1.6 - 1.6, --  down from main_gear_pos !!!
		main_gear_amortizer_reversal_stroke  = 	1.5 - 1.6, --  up 
		nose_gear_amortizer_normal_weight_stroke = -0.095,
		main_gear_amortizer_normal_weight_stroke = -0.114,
		radar_can_see_ground	=	false,
		tand_gear_max 							 = 0.3445,	

		AOA_take_off	=	0.14,
		stores_number	=	9,
		bank_angle_max	=	60,
		Ny_min	=	-2,
		Ny_max	=	5.9,
		tand_gear_max	=	0.577,
		V_max_sea_level	=	322,
		V_max_h	=	440,
		tanker_type	=	0,
		wing_area	=	49.24,
		wing_span	=	11.68,
		wing_type = 2,			
		thrust_sum_max	=	16240,
		thrust_sum_ab	=	16240,
		Vy_max	=	253,
		length	=	19.2,
		height	=	5,
		flaps_maneuver	=	1,
		Mach_max	=	2.17,
		range	=	2593,
		--crew_size	=	2,
		RCS	=	7,
		Ny_max_e	=	6,
		detection_range_max	=	100,
		IR_emission_coeff	=	1,
		IR_emission_coeff_ab	=	4,
		engines_count	=	1,
		wing_tip_pos = 	{-3.207,	-0.00,	10.2},--*
		nose_gear_wheel_diameter	=	0.754,
		main_gear_wheel_diameter	=	0.972,
		engines_nozzles = 
		{
			[1] = 
			{
				pos = 	{-3.605,	-0.65,	-0.50},--
				elevation	=	0.0,-- -1.5   winkel nach oben unten
				diameter	=	0.605,-- 0.765 cone diameter   Kreis �
				exhaust_length_ab	=	4, --lenght in m  Kreis � kegel efekt
				exhaust_length_ab_K	=	0.707,
				smokiness_level     = 	0.01, 
			}, -- end of [1]
			
		}, -- end of engines_nozzles
		crew_size	=	1,
		crew_members = 
		{
			[1] = 
			{
			ejection_seat_name	= "cache_1",
			pilot_name		   	=  "cache_4",
			drop_canopy_name	= "cache_2",
			drop_parachute_name =  "cache_3",
			pos					= {2.679, 0.512, 0.0 },
			canopy_pos			= {2.739, 0.677, 0.0},
			}, -- end of [1]
		}, -- end of crew_members
		brakeshute_name	=	3,
		is_tanker	=	false,
		air_refuel_receptacle_pos = 	{0.000,	0.000,	0.000},--9.709,	1.305,	-0.866
		fires_pos = 
		{
			[1] = 	{-1.594,	-0.064,	0},
			[2] = 	{-1.073,	0.319,	3.304},
			[3] = 	{-1.187,	0.338,	-3.678},
			[4] = 	{-0.82,	0.265,	2.774},
			[5] = 	{-0.82,	0.265,	-2.774},
			[6] = 	{-0.82,	0.255,	2.274},
			[7] = 	{-0.82,	0.255,	-2.274},
			[8] = 	{-4.889,	-0.257,	1.193},
			[9] = 	{-4.889,	0.300,	-0.0},
			[10] = 	{-1.257,	0.283,	3.05},
			[11] = 	{-1.257,	0.283,	-3.05},
		}, -- end of fires_pos
		chaff_flare_dispenser = 
		{
			[1] = 
			{
				dir = 	{0,	1,	0},
				pos = 	{-5.776,	1.4,	-0.422},
			}, -- end of [1]
			[2] = 
			{
				dir = 	{0,	1,	0},
				pos = 	{-5.776,	1.4,	0.422},
			}, -- end of [2]
		}, -- end of chaff_flare_dispenser

        LandRWCategories = 
        {
            [1] = 
            {
                Name = "AircraftCarrier",
            }, -- end of [1]
        }, -- end of LandRWCategories
		MaxFuelWeight = "15245",
        MaxHeight = "20000",
        MaxSpeed = "3000",
        MaxTakeOffWeight = "41200",
        Picture = "MQ9_PREDATOR_B.png",
        Rate = "30",
        Shape = "Bayraktar_TB2_UAV",
        TakeOffRWCategories = 
        {
            [1] = 
            {
                Name = "AircraftCarrier With Catapult",
            }, -- end of [1]
			[2] = 
            {
				Name = "AircraftCarrier With Tramplin",
            }, -- end of [2]
        }, -- end of TakeOffRWCategories
        WingSpan = "11.68",
       

    -- Countermeasures
		passivCounterm = {
			CMDS_Edit = true,
			SingleChargeTotal = 256,
			-- PPR-26
			chaff = {default = 128, increment = 32, chargeSz = 1},
			-- PPI-26
			flare = {default = 128, increment = 32, chargeSz = 1}
        },
	
        CanopyGeometry = {
            azimuth = {-145.0, 145.0},
            elevation = {-50.0, 90.0}
        },

Sensors = {
RADAR = "AN/APQ-120",
IRST = "OLS-27",
OPTIC = {"TADS DTV", "TADS DVO", "TADS FLIR"},
RWR = "Abstract RWR"
},
	Failures = {
			{ id = 'asc', 		label = _('ASC'), 		enable = false, hh = 0, mm = 0, mmint = 1, prob = 100 },
			{ id = 'autopilot', label = _('AUTOPILOT'), enable = false, hh = 0, mm = 0, mmint = 1, prob = 100 },
			{ id = 'hydro',  	label = _('HYDRO'), 	enable = false, hh = 0, mm = 0, mmint = 1, prob = 100 },
			{ id = 'l_engine',  label = _('L-ENGINE'), 	enable = false, hh = 0, mm = 0, mmint = 1, prob = 100 },
			{ id = 'r_engine',  label = _('R-ENGINE'), 	enable = false, hh = 0, mm = 0, mmint = 1, prob = 100 },
			{ id = 'radar',  	label = _('RADAR'), 	enable = false, hh = 0, mm = 0, mmint = 1, prob = 100 },
			{ id = 'eos',  		label = _('EOS'), 		enable = false, hh = 0, mm = 0, mmint = 1, prob = 100 },
			{ id = 'helmet',  	label = _('HELMET'), 	enable = false, hh = 0, mm = 0, mmint = 1, prob = 100 },
			--{ id = 'mlws',  	label = _('MLWS'), 		enable = false, hh = 0, mm = 0, mmint = 1, prob = 100 },
			{ id = 'rws',  		label = _('RWS'), 		enable = false, hh = 0, mm = 0, mmint = 1, prob = 100 },
			{ id = 'ecm',   	label = _('ECM'), 		enable = false, hh = 0, mm = 0, mmint = 1, prob = 100 },
			{ id = 'hud',  		label = _('HUD'), 		enable = false, hh = 0, mm = 0, mmint = 1, prob = 100 },
			{ id = 'mfd',  		label = _('MFD'), 		enable = false, hh = 0, mm = 0, mmint = 1, prob = 100 },		
	},
	HumanRadio = {
		frequency = 127.5,  -- Radio Freq
		editable = true,
		minFrequency = 100.000,
		maxFrequency = 156.000,
		modulation = MODULATION_AM
	},
	mapclasskey = "P0091000024",



    Guns = {gun_mount("DEFA_554", { count = 00 },{muzzle_pos = {3.10000, -0.300000, -0.450000}})

},
Pylons =     {
	pylon(1, 0, -0.666000, -1.50000, -2.345000, --33
            {
                FiZ = 0,
            },
            {
				{ CLSID = "{maml_tb2}",attach_point_position =  {0.00, 0.00000, 0.0000,},arg = 52,arg_value = 0.3 },   --GBU-1
 			}
        ),
       pylon(2, 0, -0.666000, -1.507000, -1.825000,
            {
                FiZ = 0,
            },
            {    
                { CLSID = "{maml_tb2}",attach_point_position =  {0.0, 0.00000, 0.0000,},arg = 52,arg_value = 0.3 },   --GBU-12
  			}
			
        ),
        pylon(3, 0, -0.666000, -1.507000, 2.015000,
            {	
                FiZ = 0,
            },
            {
                { CLSID = "{maml_tb2}",attach_point_position =  {0.00, 0.00000, 0.000,},arg = 52,arg_value = 0.3 },   --GBU-12
			}
        ),
        pylon(4, 0, -0.666000, -1.50000, 2.525000,
            {
                FiZ = 0,
            },
            {
				{ CLSID = "{maml_tb2}",attach_point_position =  {0.00, 0.00000, 0.0000,},arg = 52,arg_value = 0.3 },   --GBU-12
				}
        )
},
	
	EPLRS = true,
	Tasks = {
		aircraft_task(GroundAttack),
        aircraft_task(CAS),
        aircraft_task(AFAC),
		aircraft_task(Reconnaissance),
    },	
	DefaultTask = aircraft_task(GroundAttack),

	SFM_Data = {
		aerodynamics = -- Cx = Cx_0 + Cy^2*B2 +Cy^4*B4
		{
			Cy0			=	0.1,      -- zero AoA lift coefficient
			Mzalfa		=	4.355,  -- coefficients for pitch agility
			Mzalfadt	=	0.8,    -- coefficients for pitch agility
			kjx			=	2.25,    
			kjz			=	0.00125, 
			Czbe		=	-0.016, -- coefficient, along Z axis (perpendicular), affects yaw, negative value means force orientation in FC coordinate system
			cx_gear		=	0.012,    -- coefficient, drag, gear 0.0277
			cx_flap		=	0.095,   -- coefficient, drag, full flaps
			cy_flap		=	0.31,    -- coefficient, normal force, lift, flaps
			cx_brk		=	0.06,   -- coefficient, drag, breaks
			table_data  = 
			{	--        M		 Cx0	 Cya	  B		 B4	    Omxmax	   Aldop   Cymax
				[1] = 	{0,		0.024,	0.07,	0.075,	0.12,	0.5,		30,		1.2},
				[2] = 	{0.1,	0.024,	0.07,	0.075,	0.12,	1.5,		30,		1.2},
				[3] = 	{0.2,	0.024,	0.07,	0.075,	0.12,	0.79,		30,		1.2},
				[4] = 	{0.3,	0.0239,	0.073,	0.075,	0.12,	1.24,		30,		1.2},
				[5] = 	{0.4,	0.024,	0.076,	0.075,	0.12,	1.323,		28.7,	1.18},
				[6] = 	{0.5,	0.0235,	0.079,	0.075,	0.12,	1.13,		27.3,	1.16},
				[7] = 	{0.6,	0.025,	0.083,	0.075,	0.125,	0.94,		26,		1.14},
				[8] = 	{0.7,	0.044,	0.085,	0.14,	0.1,	0.67,		24.7,	1.12},
				[9] = 	{0.8,	0.0465,	0.0855,	0.1775,	0.125,	0.57,		24,		1.11},
				[10] = 	{0.9,	0.049,	0.086,	0.215,	0.15,	0.456,		18,		1.1},
				[11] = 	{1.9,	0.049,	0.083,	0.228,	0.17,	0.32,		17,		1.05},
			}, -- end of table_data
			
		}, -- end of aerodynamics
		engine = 
		{
			Nmg	=	20.5, -- RPM at idle
			MinRUD	=	0, -- Min state of the throttle
			MaxRUD	=	1, -- Max state of the throttle
			MaksRUD	=	1, -- Military power state of the throttle
			ForsRUD	=	1, -- Afterburner state of the throttle
			typeng	=	3,--PISTON ENGINE
			--[[
				E_TURBOJET = 0
				E_TURBOJET_AB = 1
				E_PISTON = 2
				E_TURBOPROP = 3
				E_TURBOFAN				= 4
				E_TURBOSHAFT = 5
			--]]
			
			hMaxEng	=	12.5, -- Max altitude for safe engine operation in km
			dcx_eng	=	0.015, -- Engine drag coeficient
			cemax	=	0.37, -- not used for fuel calulation , only for AI routines to check flight time ( fuel calculation algorithm is built in )
			cefor	=	0.37, -- not used for fuel calulation , only for AI routines to check flight time ( fuel calculation algorithm is built in )
			dpdh_m	=	1800, --  altitude coefficient for max thrust
			dpdh_f	=	1800,  --  altitude coefficient for AB thrust
			
			k_adiab_1			= 0.037923,
			k_adiab_2			= 0.0562,
			MAX_Manifold_P_1	= 155774,		
			MAX_Manifold_P_2	= 206570,		
			MAX_Manifold_P_3	= 226648,		
			k_after_cool		= 0.,
			Displ				= 35,
			k_Eps				= 6.5,
			Stroke				= 0.165,
			V_pist_0			= 13,
			Nu_0				= 1.2,
			Nu_1				= 0.9,
			Nu_2				= 0.001,
			N_indic_0			= 1052480,
			N_fr_0				= 0.04,
			N_fr_1				= 0.001,
			Init_Mom			= 220,
			D_prop				= 3.5,
			MOI_prop			= 45,
			k_gearbox			= 2.4,
			P_oil				= 495438,
			k_boost				= 3,
			k_cfug				= 0.003,
			k_oil				= 0.00004,
			k_piston			= 3000,
			k_reg				= 0.003,
			k_vel				= 0.017,
			table_data = 
			{
			--   M			Pmax
				{0.0,		16620.0},
				{0.1,		15600.0},
				{0.2,		14340.0},
				{0.3,		13320.0},
				{0.4,		12230.0},
				{0.5,		11300.0},
				{0.6,		10600.0},
				{0.7,		10050.0},
				{0.8,		 9820.0},
				{0.9,		 5902.0},
				{1.9,		 3469.0}
			}
			-- M - Mach number
			-- Pmax - Engine thrust at military power
			-- Pfor - Engine thrust at AFB
		}, -- end of engine
	},


	--damage , index meaning see in  Scripts\Aircrafts\_Common\Damage.lua
	Damage  = verbose_to_dmg_properties({
		--fuselage
		["NOSE_CENTER"]  		 = {critical_damage = 1  ,args = {148},droppable = false}, -- sensor ball 
		["NOSE_TOP"]  	 		 = {critical_damage = 2  ,args = {147}},
		["NOSE_Bottom"]  		 = {critical_damage = 2  ,args = {147}},
		["FUSELAGE_TOP"] 	  	 = {critical_damage = 5  ,args = {151}},
		["FUSELAGE_BOTTOM"] 	 = {critical_damage = 5  ,args = {152}},
	
		["TAIL_TOP"]  	 		 = {critical_damage = 5	 ,args = {115}},
		["TAIL_BOTTOM"]  		 = {critical_damage = 5  ,args = {156}},
		
		["FRONT_GEAR_BOX"]  	 = {critical_damage = 5  ,},
		["LEFT_GEAR_BOX"]  	 	 = {critical_damage = 5  ,},
		["RIGHT_GEAR_BOX"]  	 = {critical_damage = 5  ,},

		
		["ROTOR"] 				 = {critical_damage = 3  ,args = {271},deps_cells = {"BLADE_1_OUT","BLADE_2_OUT","BLADE_3_OUT"}},
		["BLADE_1_OUT"] 		 = {critical_damage = 1  ,droppable = false},
		["BLADE_2_OUT"] 		 = {critical_damage = 1  ,droppable = false},
		["BLADE_3_OUT"] 		 = {critical_damage = 1  ,droppable = false},

		["STABILIZATOR_L_IN"]	 = {critical_damage = 5  ,args = {246},deps_cells = {"ELEVATOR_L_IN","ELEVATOR_L_OUT"}},
		["ELEVATOR_L_IN"]	 	 = {critical_damage = 2  ,args = {239},droppable = false},
		["ELEVATOR_L_OUT"]	 	 = {critical_damage = 2  ,args = {240},droppable = false},
		["STABILIZATOR_R_IN"]	 = {critical_damage = 5  ,args = {243},deps_cells = {"ELEVATOR_R_IN","ELEVATOR_R_OUT"}},
		["ELEVATOR_R_IN"]	 	 = {critical_damage = 2  ,args = {237},droppable = false},
		["ELEVATOR_R_OUT"]	     = {critical_damage = 2  ,args = {238},droppable = false},

		["RUDDER_R"]	 		 = {critical_damage = 3  ,args = {247},deps_cells = {"RUDDER"}},
		["RUDDER"]	 			 = {critical_damage = 1  ,args = {224}},
		--left wing
		["WING_L_OUT"]	 		 = {critical_damage = 5  ,args = {213},deps_cells = {"FLAPS_L_OUT"	,"WING_L_CENTER"}},
		["WING_L_CENTER"] 		 = {critical_damage = 5  ,args = {214},deps_cells = {"FLAPS_L_CENTER","FLAPS_L_IN","WING_L_IN"}},
		["WING_L_IN"] 			 = {critical_damage = 5  ,args = {223},deps_cells = {"AILERON_L"},droppable = false},
		["FLAPS_L_OUT"]	 		 = {critical_damage = 2  ,args = {226},droppable = false},
		["FLAPS_L_CENTER"] 		 = {critical_damage = 2  ,args = {227},droppable = false},
		["FLAPS_L_IN"]	 		 = {critical_damage = 2  ,args = {228},droppable = false},
		["AILERON_L"] 			 = {critical_damage = 2  ,args = {229},droppable = false},
		--right wing	
		["WING_R_OUT"]	 		 = {critical_damage = 5  ,args = {213},deps_cells = {"FLAPS_R_OUT"	,"WING_R_CENTER"}},
		["WING_R_CENTER"] 		 = {critical_damage = 5  ,args = {214},deps_cells = {"FLAPS_R_CENTER","FLAPS_R_IN","WING_R_IN"}},
		["WING_R_IN"] 			 = {critical_damage = 5  ,args = {215},deps_cells = {"AILERON_R"},droppable = false},
		["FLAPS_R_OUT"]	 		 = {critical_damage = 2  ,args = {216},droppable = false},
		["FLAPS_R_CENTER"] 		 = {critical_damage = 2  ,args = {217},droppable = false},
		["FLAPS_R_IN"]	 		 = {critical_damage = 2  ,args = {218},droppable = false},
		["AILERON_R"] 		     = {critical_damage = 2  ,args = {219},droppable = false},
	}),
	
	DamageParts = 
	{  
		[1] = "mq-9_reaper_oblomok_R", -- wing R
		[2] = "mq-9_reaper_oblomok_L", -- wing L
	},
	
	lights_data = {	typename = "collection", lights = {
    [3]	= {typename = "collection",
			lights = {-- Left Position Light (red)
					  {typename = "omnilight",
					   connector = "BANO_1",
					   color = {0.99, 0.11, 0.3},
					   pos_correction  = {0, 0, -0.2},
					   argument  = 190
					  },
					  -- Right Position Light (green)
					  {typename = "omnilight",
					   connector = "BANO_2",
					   color = {0, 0.894, 0.6},
					   pos_correction = {0, 0, 0.2},
					   argument  = 191
					  }}
			},
	
                    				
                    				
					
					
					
			
		
		
			[2] = { typename = "collection", -- form lights aft
				lights = {
					
					
					
					  {typename = "spotlight", connector = "MAIN_SPOT_PTR", argument = 208,
                            proto = lamp_prototypes.FPP_7,
                            movable = true},
							
						{
                            typename = "spotlight", connector = "MAIN_SPOT_PTR",
                            proto = lamp_prototypes.FPP_7_halo,
                            movable = true },
                       	
							 {
                            typename = "omnilight", connector = "MAIN_SPOT_PTR", pos_correction = {0.25, 0.0, 0.0},
                            proto = lamp_prototypes.FPP_7, range = 8.0,
                            movable = true},
                 
							
							
							
							
					 
				},
			},
			[3] = { typename = "collection", -- left nav light
				lights = {
					
					{typename = "spotlight", connector = "BANO_1", dir_correction = {elevation = math.rad(-45.0)}, argument = 49,
                           proto = lamp_prototypes.BANO_7M_red},
					
					 
                      --     { typename = "spotlight", connector = "BANO_2", dir_correction = {elevation = math.rad(45.0)}, argument = 191,
                         --   proto = lamp_prototypes.BANO_7M_green},
                        
					
					 
                       --    { typename = "spotlight", connector = "BANO_0", dir_correction = {azimuth = math.rad(180.0)}, argument = 192,
                        --    proto = lamp_prototypes.HS_2A },
                     
					
					
					
					
					
					
				},
			},
			[4] = { typename = "collection", -- tail nav light
				lights = {
				-- {typename = "argnatostrobelight",connector = "RED_BEACON",argument = 195,period = 2.0,color = {1.0, 0.0, 0.0},phase_shift = 0.0},	
				-- {typename = "argnatostrobelight",connector = "RED_BEACON",argument = 196,period = 2.0,color = {1.0, 0.0, 0.0},phase_shift = 0.0},	
				-- { typename = "RotatingBeacon", connector = "RED_BEACON", argument = 193,proto = lamp_prototypes.MSL_3_2, emitter_shift_x = -0.25},	
					{typename = "argnatostrobelight",connector = "RED_BEACON R",argument = 193,period = 2.0,color = {1.0, 0.0, 0.0},phase_shift = 0.0},
					{typename = "argnatostrobelight",connector = "RED_BEACON R",argument = 194,period = 2.0,color = {1.0, 0.0, 0.0},phase_shift = 0.0},
					{typename = "argnatostrobelight",connector = "RED_BEACON R",argument = 195,period = 2.0,color = {1.0, 0.0, 0.0},phase_shift = 0.0},
					{typename = "argnatostrobelight",connector = "RED_BEACON R",argument = 196,period = 2.0,color = {1.0, 0.0, 0.0},phase_shift = 0.0},
						},
			},
			[5] = { typename = "collection", -- tail nav light
				lights = {
					--{typename = "spotlight",argument = 0}, -- FORMATION LIGHTS   
					--{typename = "spotlight",connector = "MAIN_SPOT_PTL",argument_1 = 208,period = 2.0,color = {1.0, 0.0, 0.0},phase_shift = 0.0},
						
					
					
					
					
				},
			},
		}
	}, -- end lights_data
}

add_aircraft(Bayraktar_TB2_UAV)





