// Dauphin AS 365N configuration file
// Original by Antti Pankkonen
// External repain by Florian LAROYE
// Cockpit by Fabien VENRIES
[fltsim.0]
title=AS 365N2 Marine SP
sim=DauphinN2
visual_damage=1
model=
panel=
sound=
texture=
kb_checklists=check_list\AS365_check_IFR
kb_reference=check_list\AS365_ref
atc_id=91
atc_model=AS 362
ui_manufacturer=Aerospatiale
ui_type=AS 365N2 Dauphin Photorealist
ui_variation=Marine
prop_anim_ratio=1.41
description=Conçu à partir du AS 360C Dauphin, propulsé par un turbomoteur Turbomeca Astazou et équipé d'un train d'atterrissage fixe, le AS 365 Dauphin 2 est doté de deux turbomoteurs Turbomeca Arriel et d'un atterrisseur escamotable. Une version de cet appareil, désignée AS 365F et detinée aux missions de recherche et de sauvetage, est pourvue d'un radar de recherche Thomson-CSF ORB 32 Heracles II ou Bendix RDR 1500, d'un pilote automatique, d'un système de navigation sophistiqué Crouzet ONS 200A et d'un treuil servant au repêchage des naufragés et pouvant emporter une charge de 275 kg au bout d'une élingue de 90 m. L'US Coast Guard a pris en compte une autre variante de Dauphin 2, le AS 366G-1, sous la désignation de HH-65A Dolphin.
atc_heavy=0
atc_airline=MARINE
atc_flight_number=
[General]
atc_type=AEROSPATIALE
atc_model=AS365
performance=Equipage mini : 1 pilote (2 en IFR)\nPassagers : 14 (équipage inclus)\n\nMasse en charge : 4000 Kg\nMasse mini : 2300 Kg\nElingue : 1600 Kg\nTreuil charge max : 272 Kg\nVitesse max (Vne) : 175 Kts\nVitesse de croisière : 145 Kts\nAltitude temp. approuvées : 15000 ft\nDiamètre rotor : 11m68\nLongueur : 13m35\nHauteur : 3m81\nVitesse de rotation rotor : 350 tr\/mn\nRéservoirs princ. : l\nRéservoir sup de soute : 180 l\nLargage carburant : 6 mn\n\n2 Turbomoteurs Arriel 1c2\nPuissance : 980 Cv
[WEIGHT_AND_BALANCE]
max_gross_weight = 9369.000
empty_weight = 5007.000
reference_datum_position = 0.000, 0.000, 0.000
empty_weight_CG_position = 0.000, 0.000, 0.000
max_number_of_stations = 14
station_load.0 =170.000000, -0.720000, 1.400000, 3.200000, Pilote
station_load.1 =0.000000, -0.720000, -1.400000, 3.200000, Co-Pilote
station_load.2 = "0, -1.0, -1.42, 3.0, Passager 1" // Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.3 = "0, -1.0, -1.09, 3.0, Passager 2" // Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.4 = "0, -1.0, 1.09, 3.0, Passager 3" // Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.5 = "0, -1.0, 1.42, 3.0, Passager 4" // Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.6 = "0, -1.3, -1.42, 3.0, Passager 5" // Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.7 = "0, -1.3, -1.09, 3.0, Passager 6" // Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.8 = "0, -1.3, 1.09, 3.0, Passager 7" // Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.9 = "0, -1.3, 1.42, 3.0, Passager 8" // Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.10 = "0, -1.3, -1.42, 3.0, Passager 9" // Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.11 = "0, -1.5, -1.09, 2.6, Baggages" // Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
;Moments of Inertia
empty_weight_pitch_MOI = 15800.000
empty_weight_roll_MOI = 13200.000
empty_weight_yaw_MOI = 16800.000
empty_weight_coupled_MOI = 0.000
CG_forward_limit= 0.000
CG_aft_limit= 1.000
//
//-----Fuel quantity is set to 1/3 of the real aircraft -
//-----to get fuel flow and range to match those of real thing. -
//-----Gauges are scaled to display correct values. -
//
[turboprop_engine]
power_scalar=1.0
[propeller]
thrust_scalar=1.0
propeller_type=1
propeller_diameter=6.883000
propeller_blades=2
propeller_moi=5.706520
beta_max=0.000000
beta_min=15.000000
min_gov_rpm=0.000000
prop_tc=0.100000
gear_reduction_ratio=1.000000
fixed_pitch_beta=20.000000
low_speed_theory_limit=80.000000
prop_sync_available=0
prop_deice_available=0
prop_feathering_available=0
prop_auto_feathering_available=0
min_rpm_for_feather=0.000000
beta_feather=0.000000
power_absorbed_cf=0.000000
defeathering_accumulators_available=0
prop_reverse_available=0.000000
minimum_on_ground_beta=0.000000
minimum_reverse_beta=0.000000
[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, 5 , 17.0
avionics = 1, 5 , 17.0
pitot_heat = 0, 2 , 17.0
max_battery_voltage= 27.9
additional_system = 0, 2 , 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
[contact_points]
//0 Class <0=none,1=wheel, 2=scrape, 3=skid>
//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)
static_pitch= -5.000
static_cg_height= 2.294
point.0= 1.000, -21.200, 0.000, -1.400, 1500.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000
point.1= 1.000, 9.250, 0.000, -2.560, 1378.000, 1.000, 0.984, 38.000, 0.960, 1.250, 0.923, 2.500, 2.500, 0.000, 125.000, 125.000
point.2= 1.000, 9.250, 0.000, -2.560, 1378.000, 2.000, 0.984, 38.000, 0.960, 1.250, 0.923, 2.500, 2.500, 0.000, 125.000, 125.000
point.3= 1.000, -3.000, -3.330, -3.380, 1378.000, 1.000, 1.148, 0.000, 0.860, 1.350, 0.933, 3.000, 3.000, 0.000, 125.000, 125.000
point.4= 1.000, -3.000, 3.330, -3.380, 1378.000, 2.000, 1.148, 0.000, 0.860, 1.350, 0.933, 3.000, 3.000, 0.000, 125.000, 125.000
point.5= 2.000, 11.000, 0.000, 1.000, 1000.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 4.000, 0.000, 0.000
point.6= 2.000, -22.000, 0.000, 1.500, 1000.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 9.000, 0.000, 0.000
point.7= 2.000, 0.000, -19.000, 7.300, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 5.000, 0.000, 0.000
point.8= 2.000, 0.000, 19.000, 7.300, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 6.000, 0.000, 0.000
gear_system_type=0
[brakes]
toe_brakes_scale=1.915586
parking_brake=1
[hydraulic_system]
normal_pressure=0.000000
[Views]
eyepoint=-0.72,1.4,3.2
[lights]
//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing
light.0=3, -16.6, -5.30, 0.90, fx_navred ,
light.1=3, -16.6, 5.30, 0.90, fx_navgre ,
light.2=3, -25.4, 0.00, 0.90, fx_navwhi ,
light.3=2, -24.2, -0.20, 9.30, fx_beacon ,
light.4=4, 1.00, -1.00, 1.50, fx_vclight ,
light.5=4, 1.00, 1.00, 1.50, fx_vclight ,
light.6=4, -4.50, 0.00, 1.30, fx_vclight ,
light.9=4, 7.30, -1.35, 2.60, fx_vclight ,
light.10=4, 7.30, 1.35, 2.60, fx_vclight ,
[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, 1
Adf.1=1
Transponder.1=1
Marker.1=1
[keyboard_response]
elevator=100.000000,180.000000
aileron=200.000000,1000.000000
rudder=200.000000,1000.000000
[direction_indicators]
direction_indicator.0=3,0
[attitude_indicators]
attitude_indicator.0=1
[turn_indicators]
turn_indicator.0=1,0
[effects]
wake=fx_wake
water=fx_spray
dirt =fx_tchdrt
concrete = fx_sparks
touchdown = fx_tchdwn_s, 1
[fuel]
Center1= 0.000, 0.000, 0.000, 100.000, 0.000
fuel_type=2.000000
number_of_tank_selectors=2
LeftMain=0,000000,0,000000,0,000000,150,000000,0,000000
RightMain=0,000000,0,000000,0,000000,150,000000,0,000000
electric_pump=0
[GeneralEngineData]
engine_type= 3
Engine.0= -0.833, -20.000, 60.000
Engine.1= -0.833, -20.000, 60.000
fuel_flow_scalar=3.0
min_throttle_limit=0.000000
[Reference Speeds]
flaps_up_stall_speed=0.000000
full_flaps_stall_speed=0.000000
cruise_speed=141.000000
max_indicated_speed=182.000000
[autopilot]
autopilot_available=1
flight_director_available=1
default_vertical_speed=1800,000000
autothrottle_available=1
pitch_takeoff_ga=0.000000
autothrottle_arming_required=1
autothrottle_takeoff_ga=0
autothrottle_max_rpm=90.000000
max_pitch=10.000000
max_pitch_acceleration=1.000000
max_pitch_velocity_lo_alt=2.000000
max_pitch_velocity_hi_alt=1.500000
max_pitch_velocity_lo_alt_breakpoint=20000.000000
max_pitch_velocity_hi_alt_breakpoint=28000.000000
max_bank=25.000000
max_bank_acceleration=1.800000
max_bank_velocity=3.000000
max_throttle_rate=0.100000
nav_proportional_control=9.000000
nav_integrator_control=0.250000
nav_derivative_control=0.000000
nav_integrator_boundary=2.500000
nav_derivative_boundary=0.000000
gs_proportional_control=9.520000
gs_integrator_control=0.260000
gs_derivative_control=0.000000
gs_integrator_boundary=0.700000
gs_derivative_boundary=0.000000
yaw_damper_gain=0.000000
[yaw_string]
yaw_string_available=1
[Helicopter]
correlator_available = 1
governed_pct_rpm_ref = 1.04
governor_pid = 0.4, 0, 0.1, 0, 0.2
rotor_brake_scalar = 1.0
torque_scalar = 1.0
cyclic_roll_control_scalar =1.0
cyclic_pitch_control_scalar =1.0
pedal_control_scalar =1.0
collective_on_rotor_torque_scalar = 1.0
[exits]
number_of_exits=1
exit_rate.0=0.4
[smokesystem]
smoke.0=2.00, -7.00, -1.70, fx_helismAS365
smoke.1=2.00, -7.00, 1.70, fx_helismAS365
[gear_warning_system]
gear_warning_available=0
pct_throttle_limit=0.000000
flap_limit_power=0.000000
flap_limit_idle=0.000000
[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
