[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
