[fltsim.0] title=HM Bark Endeavour sim=HMBark model= panel= sound= texture= kb_checklists= kb_reference= atc_id=NTECJ ui_manufacturer=Royal Navy ui_type=Bark ui_variation=H M Bark Endeavour description=Enter your description here. atc_heavy=0 atc_airline= atc_flight_number= [General] atc_type= atc_model= performance=Enter your performance information here. [fltsim.1] title=HM Bark Endeavour moored sim=HMBark model=m panel= sound= texture= kb_checklists= kb_reference= atc_id=NTECJ ui_manufacturer=Royal Navy ui_type=Bark ui_variation=H M Bark Endeavour furled sails description=Enter your description here. atc_heavy=0 atc_airline= atc_flight_number= [WEIGHT_AND_BALANCE] max_gross_weight = 8035.000 empty_weight = 4265.000 reference_datum_position = 13.100, 0.000, 0.000 empty_weight_CG_position = -14.200, 0.000, -50.000 max_number_of_stations = 50 station_load.0 = 170.000, -11.300, -1.500, -50.000 station_load.1 = 170.000, -11.300, 1.500, -50.000 station_load.2 = 170.000, -13.900, 1.500, -50.000 station_load.3 = 170.000, -13.900, -1.500, -50.000 ;Moments of Inertia empty_weight_pitch_MOI = 1800000.000 empty_weight_roll_MOI = 5500000.000 empty_weight_yaw_MOI = 16.000 empty_weight_coupled_MOI = 0.000 CG_forward_limit= 0.000 CG_aft_limit= 1.000 [exits] number_of_exits = 2 exit_rate.0 = 0.4 ;Percent per second exit_rate.1 = 0.4 ;Percent per second [electrical] max_battery_voltage = 12.0 generator_alternator_voltage = 13.8 max_generator_alternator_amps = 40.0 ;BusType, MaxAmpLoad, MinVoltage BusTypes:0=MainBus,1=AvionicsBus,2=BatteryBus,3=HotBatteryBus,4-7=Generator/AlternatorBus(1-4) avionics_bus = 0, 10, 9.5 avionics = 1, 5 , 9.5 additional_system = 0, 20, 9.5 marker_beacon = 1, 2 , 9.0 fuel_pump = 0, 5 , 9.0 [flight_tuning] cruise_lift_scalar =1.000 parasite_drag_scalar =0.101 induced_drag_scalar =4500.001 elevator_effectiveness =1.000 aileron_effectiveness =1.000 rudder_effectiveness =100.001 pitch_stability =1.000 roll_stability =1.000 yaw_stability =1.000 elevator_trim_effectiveness =1.000 aileron_trim_effectiveness =1.000 rudder_trim_effectiveness =100.001 [GeneralEngineData] engine_type = 1 Engine.0 = -1.300, 0.000, -48.000 fuel_flow_scalar = 0.001 [TurbineEngineData] fuel_flow_gain = 0.003 inlet_area = 23.200 rated_N2_rpm = 32920.000 static_thrust = 5790.000 afterburner_available = 0 reverser_available = 1 [jet_engine] thrust_scalar =1.000 //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= 4.000, 14.000, -5.250, -48.500, 50000.100, 0.000, 0.000, 0.000, 0.550, 2.500, 0.650, 0.000, 0.000, 0.000, 0.000, 0.000 point.1= 4.000, 14.000, 5.250, -48.500, 50000.100, 0.000, 0.000, 0.000, 0.550, 2.500, 0.650, 0.000, 0.000, 0.000, 0.000, 0.000 point.2= 4.000, -68.350, -5.250, -48.500, 50000.100, 0.000, 0.000, 0.000, 0.550, 2.500, 0.650, 0.000, 0.000, 0.000, 0.000, 0.000 point.3= 4.000, -68.350, 5.250, -48.500, 50000.100, 0.000, 0.000, 0.000, 0.550, 2.500, 0.650, 0.000, 0.000, 0.000, 0.000, 0.000 point.4= 3.000, 14.000, -5.250, -48.500, 50000.100, 0.000, 0.000, 0.000, 0.550, 2.500, 0.650, 0.000, 0.000, 0.000, 0.000, 0.000 point.5= 3.000, 14.000, 5.250, -48.500, 50000.100, 0.000, 0.000, 0.000, 0.550, 2.500, 0.650, 0.000, 0.000, 0.000, 0.000, 0.000 point.6= 3.000, -68.350, -5.250, -48.500, 50000.100, 0.000, 0.000, 0.000, 0.550, 2.500, 0.650, 0.000, 0.000, 0.000, 0.000, 0.000 point.7= 3.000, -68.350, 5.250, -48.500, 50000.100, 0.000, 0.000, 0.000, 0.550, 2.500, 0.650, 0.000, 0.000, 0.000, 0.000, 0.000 point.8= 1.000, -1.150, -5.250, 7.800, 16000.100, 0.000, 0.010, 30.000, 0.350, 2.500, 0.800, 12.000, 12.000, 0.000, 0.000, 0.000 static_pitch = 0.000 static_cg_height = 48.500 [Views] eyepoint = -55.91, -4.91, -32.0 [Radios] // Radio Type = availiable, standby frequency, has glide slope Audio.1 = 1 Com.1 = 1, 0 Nav.1 = 1, 0, 1 Nav.2 = 1, 0, 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 [EFFECTS] wake=fx_wake, 0.0, 0.0 ,120.6 water=fx_sink_sm, 0.0, 0.0, 120.6 dirt= concrete= touchdown= [fuel] Center1 = -15.300, 0.000, -55.500, 1660.000, 3.600 LeftMain = -36.300, -10.000, -55.500, 268.500, 0.000 RightMain = -36.300, 10.000, -55.500, 268.500, 0.000 fuel_type = 2 //Fuel type: 1 = Avgas, 2 = JetA number_of_tank_selectors = 1 [airplane_geometry] wing_area = 279.000 wing_span = 52.100 wing_root_chord = 6.400 wing_dihedral = 3.900 wing_incidence = 2.500 wing_twist = -1.700 oswald_efficiency_factor= 0.700 wing_winglets_flag = 0 wing_sweep = 0.000 wing_pos_apex_lon = -28.000 wing_pos_apex_vert = 0.000 htail_area = 39.000 htail_span = 11.700 htail_pos_lon = -27.800 htail_pos_vert = -50.000 htail_incidence = 2.000 htail_sweep = 5.000 vtail_area = 18.000 vtail_span = 4.800 vtail_sweep = 45.000 vtail_pos_lon = -25.700 vtail_pos_vert = -50.500 elevator_area = 16.600 aileron_area = 18.300 rudder_area = 66.700 elevator_up_limit = 28.000 elevator_down_limit = 21.000 aileron_up_limit = 20.000 aileron_down_limit = 15.000 rudder_limit = 42.000 elevator_trim_limit = 19.500 spoiler_limit = 20.000 spoilerons_available = 1 aileron_to_spoileron_gain = 4.600 min_ailerons_for_spoilerons = 5.000 min_flaps_for_spoilerons= 0.000 [Reference Speeds] flaps_up_stall_speed = 100.000 full_flaps_stall_speed = 80.000 cruise_speed = 464.000 [autopilot] autopilot_available= 1 flight_director_available= 1 default_vertical_speed= 1800.0 autothrottle_available= 1 autothrottle_arming_required= 0 autothrottle_max_rpm = 90 autothrottle_takeoff_ga= 0 pitch_takeoff_ga = 8; [forcefeedback] stick_shaker_magnitude=5000 ; 0 - 10000 stick_shaker_direction=0 ; 0 - 35999 degrees stick_shaker_period=111111 ; in microseconds 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=9000 ; 0 - 35999 degrees gear_bump_left_duration=250000 ; in microseconds gear_bump_right_magnitude=2700 ; 0 - 10000 gear_bump_right_direction=27000 ; 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= 1 span-outboard= 0.500 extending-time= 12.000 system_type= 0 damaging-speed= 250.000 blowout-speed= 300.000 lift_scalar= 1.000 drag_scalar= 1.000 pitch_scalar= 1.000 flaps-position.0= 0.000, 0.000 flaps-position.1= 8.000, 0.000 flaps-position.2= 20.000, 0.000 flaps-position.3= 40.000, 0.000