//********************************************************
//
//                       Caudron C 450
//                       version beta avril 2008
//
//  modиle de vol  Jean-Pierre Bourgeois "Bee Gee" & Benoit Dubй
//
//                       
//                        
//                        
//
//********************************************************
[fltsim.0]
title=Caudron C450
sim=caudron460-3
model=
panel=
sound=
texture=
kb_checklists=
kb_reference=
atc_id=
ui_manufacturer=Caudron-Renault
ui_type=C450
ui_variation=Coupe Deutsch 1934- Maurice Arnoux
description=Vainqueur de la coupe Deutsch en avril 1934 pilotй par Maurice Arnoux/ record du monde de vitesse (445 km/h) en aoыt 1934 pilotй par Hйlиne Boucher
atc_id_color=0x00000000
atc_heavy=0
atc_id_font=Verdana,-11,1,600,0
visual_damage=0

[fltsim.1]
title=Caudron C450 H Boucher
sim=caudron460-3
model=HBoucher
panel=
sound=
texture=HBoucher
kb_checklists=
kb_reference=
atc_id=
ui_manufacturer=Caudron-Renault
ui_type=C450
ui_variation=Record Aoыt 1934- Helиne Boucher
description=Vainqueur de la coupe Deutsch en avril 1934 pilotй par Maurice Arnoux/ record du monde de vitesse (445 km/h) en aoыt 1934 pilotй par Hйlиne Boucher
atc_id_color=0x00000000
atc_heavy=0
atc_id_font=Verdana,-11,1,600,0
visual_damage=0



[General]
atc_type= 
atc_model= 
editable=0 
performance=Vmax 450 km\/h  240 kt\n\n 

[weight_and_balance]

// ACM V2.5
max_gross_weight = 2000
empty_weight = 1150
reference_datum_position = 0, 0, 0
empty_weight_CG_position = 4.5, 0, -0.2
empty_weight_pitch_MOI = 1500
empty_weight_roll_MOI = 500
empty_weight_yaw_MOI = 1800
empty_weight_coupled_MOI = 0
max_number_of_stations = 1

station_load.0 = 170, -1.56, 0, -0.22


[GeneralEngineData]

//0=Piston, 1=Jet, 2=None, 3=Helo-Turbine, 4=Rocket, 5=Turboprop
engine_type = 0
fuel_flow_scalar = 1.0
min_throttle_limit = 0.000000
engine.0 = 11.03, 0, -0.03,

[effects]
wake = fx_wake
water = fx_spray
dirt = fx_tchdrt
concrete = fx_sparks
touchdown = fx_tchdwn_s, 1
windshield_rain_effect_available = 1

//*********************************************************************
[SMOKESYSTEM]

smoke.0= 3.0,    6.0,    0.00,     fx_caudron_smoke
smoke.1= 3.0,    12.0,    0.00,    fx_caudron_smokeVC



//***************************************************************************

[fuel]

//Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)

fuel_type = 1
number_of_tank_selectors = 1
electric_pump = 1

Center1 = 4.39, 0, -0.18, 65, 0


 
//0  Classe                       1=train, 2=structure, 3=patins  , 4=flotteurs, 5=gouvernail flotteurs 
//1  Position longitudinale       (pieds)
//2  Position laterale            (pieds)
//3  Position verticale           (pieds)
//4  Seuil domage impact          (pieds par Minute)
//5  carte des freins             (0=aucun, 1=gauche, 2=droite)
//6  Rayon pneus                  (pieds)
//7  Angle braquage               (degrees)
//8  Compression statique         (pieds)(0 si rigide)
//9  Ratio Compression Max/Statique 
//10 Ratio amortissement          (0=non amirti, 1=amortissement critique)
//11 Temps sortie train           (secondes)
//12 Temps rentree train          (secondes)
//13 Type sons                    0=train centre,1=train aux.,2=train gauche,3=train droit,4=structure fuselage,5=structure aile gauche,6=structure aile droite,7=structure aux1,8=structure aux2,9=structure queue
//14 Vitesse limite rentre train  (KIAS)
//15 Vitesse domage train         (KIAS)



[contact_points]
static_pitch = 9.05
static_cg_height = 3.35
tailwheel_lock = 0
gear_system_type = 1            // 0:train rentrant  1:train fixe
max_number_of_points = 9

point.0 = 3, -10.13, 0, -2.05, 1500, 0, 0.1, 30, 0.1, 1, 0.794, 0, 0, 0, 0, 0
point.1 = 1,   4.80, -3.02, -4.63, 2000, 1, 0.64,  0, 0.286, 2.5, 0.808, 6, 7, 2, 0, 0
point.2 = 1,   4.80,  3.02, -4.63, 2000, 2, 0.64,  0, 0.286, 2.5, 0.808, 7, 6, 3, 0, 0
point.3 = 2, 4.1181, -11.0267, -1.1796, 1574.8, 0, 0, 0, 0, 0, 0, 0, 0, 5, 0, 0
point.4 = 2, 4.1243, 11.0302, -1.1589, 0, 0, 0, 0, 0, 0, 0, 0, 6, 6, 0, 0
point.5 = 2, 11.8501, 0, 0.0086, 1574.8, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0
point.6 = 2, -11.8032, 0, -0.6786, 1574.8, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0
point.7 = 2, -9.6673, 0, 3.4193, 1574.8, 0, 0, 0, 0, 0, 0, 0, 0, 7, 0, 0
point.8 = 2, 10.0453, 0, -2.0252, 1574.8, 0, 0, 0, 0, 0, 0, 0, 0, 8, 0, 0


[keyboard_response]
elevator = 100, 180
aileron = 200, 1000
rudder = 200, 1000


[forcefeedback]
gear_bump_nose_magnitude = 3000
gear_bump_nose_direction = 18000
gear_bump_nose_duration = 250000
gear_bump_left_magnitude = 2700
gear_bump_left_direction = 35500
gear_bump_left_duration = 250000
gear_bump_right_magnitude = 2700
gear_bump_right_direction = 00500
gear_bump_right_duration = 250000
ground_bumps_magnitude1 = 1300
ground_bumps_angle1 = 08900
ground_bumps_intercept1 = 3.0
ground_bumps_slope1 = 0.20
ground_bumps_magnitude2 = 200
ground_bumps_angle2 = 09100
ground_bumps_intercept2 = 1.075
ground_bumps_slope2 = 0.035
crash_magnitude1 = 10000
crash_direction1 = 01000
crash_magnitude2 = 10000
crash_direction2 = 9000
crash_period2 = 75000
crash_duration2 = 2500000

[airplane_geometry]
//ACM_AREAW1// 0,0,0.0197,1.5096,0.3249,0.3249,0.0186,1.5075,0.9161,0.9161
//ACM_AREAW2// 0.0944,1.3869,1.3019,1.3019,0.1377,1.3050,1.6756,1.6756,0.1862,1.2295
//ACM_AREAW3// 2.2344,2.2344,0.2496,1.1124,2.6015,2.6015,0.2885,1.0305,3.0490,3.0490
//ACM_AREAW4// 0.3370,0.9484,3.1944,3.1944,0.3576,0.8639,3.3571,3.3571,0.4451,0.6011
//ACM_AREAH1// 0.0031,0.0031,0,0.5213,0.1465,0.1465,0.0498,0.5206,0.2495,0.2495
//ACM_AREAH2// 0.0684,0.5170,0.3621,0.3621,0.0996,0.5195,0.4963,0.4963,0.1404,0.5188
//ACM_AREAH3// 0.6492,0.6492,0.1808,0.5213,0.8241,0.8241,0.2213,0.5238,0.9897,0.9897
//ACM_AREAH4// 0.2684,0.5231,0.9958,0.9958,0.2653,0.6880,1.1396,1.1396,0.3558,0.5188
//ACM_AREAV1// 0.0065,0.0065,0,0.4363,0.1120,0.1120,0,0.4377,0.2171,0.2171
//ACM_AREAV2// 0.0560,0.4424,0.3095,0.3095,0.0859,0.4406,0.4214,0.4214,0.1155,0.4420
//ACM_AREAV3// 0.5468,0.5468,0.1553,0.4467,0.6916,0.6916,0.1914,0.4350,0.7807,0.7807
//ACM_AREAV4// 0.2178,0.4365,0.7835,0.7835,0.2178,0.7088,0.9549,0.9549,0.3303,0.4823
//ACM_CAREAW1// 1.9340,1.9340,0.8585,1.1719,2.1375,2.1375,0.8327,1.1308,2.3261,2.3261
//ACM_CAREAW2// 0.8123,1.0922,2.4525,2.4525,0.7990,1.0657,2.5687,2.5687,0.7886,1.0398
//ACM_CAREAW3// 2.6651,2.6651,0.7753,1.0211,2.7941,2.7941,0.7649,0.9900,2.8705,2.8705
//ACM_CAREAW4// 0.7566,0.9811,2.9298,2.9298,0.7462,0.9674,3.0536,3.0536,0.7379,0.9387
//ACM_CAREAH1// 0.1615,0.1615,0.5296,0.8079,0.2293,0.2293,0.5271,0.7978,0.3149,0.3149
//ACM_CAREAH2// 0.5271,0.7853,0.4300,0.4300,0.5271,0.7727,0.5425,0.5425,0.5271,0.7552
//ACM_CAREAH3// 0.6653,0.6653,0.5296,0.7300,0.7505,0.7505,0.5271,0.7225,0.8133,0.8133
//ACM_CAREAH4// 0.5220,0.7099,0.9060,0.9060,0.5220,0.7001,0.9889,0.9889,0.5271,0.6875
//ACM_CAREAV1// 0.0263,0.0263,0.4494,0.9749,0.1252,0.1252,0.4460,0.9409,0.2603,0.2603
//ACM_CAREAV2// 0.4460,0.8905,0.3689,0.3689,0.4426,0.8532,0.4611,0.4611,0.4426,0.8223
//ACM_CAREAV3// 0.5533,0.5533,0.4460,0.7983,0.5993,0.5993,0.4426,0.7777,0.6582,0.6582
//ACM_CAREAV4// 0.4395,0.7634,0.7174,0.7174,0.4395,0.7361,0.7667,0.7667,0.4395,0.7185
wing_area = 75.24
wing_span = 36.09
wing_root_chord = 4.97
wing_dihedral = 5.5
wing_incidence = 2.5
wing_twist = -1.5
oswald_efficiency_factor = 0.6
wing_winglets_flag = 0
wing_sweep = 6
wing_pos_apex_lon = 5.86
wing_pos_apex_vert = 0
htail_area = 9.10
htail_span = 7.48
htail_pos_lon = -7.05
htail_pos_vert = 0
htail_incidence = 1.0
htail_sweep = 15
vtail_area = 3.50
vtail_span = 3.16
vtail_sweep = 15
vtail_pos_lon = -8.42
vtail_pos_vert = 0.14
elevator_area = 4.0
aileron_area = 6.30
rudder_area = 3.20
elevator_up_limit = 25
elevator_down_limit = 25
aileron_up_limit = 20.0
aileron_down_limit = 15.0
rudder_limit = 30.0
elevator_trim_limit = 5   
spoiler_limit = 90.0
aileron_to_spoileron_gain = 0
spoiler_handle_available = 1
min_ailerons_for_spoilerons = 0
min_flaps_for_spoilerons = 0
spoilerons_available = 0

[electrical]
max_battery_voltage = 24
generator_alternator_voltage = 28
max_generator_alternator_amps = 60
engine_generator_map = 1
electric_always_available = 0
flap_motor = 0, 5, 17
gear_motor = 0, 5, 17
autopilot = 0, 5, 17
avionics_bus = 0, 10, 17
avionics = 1, 5, 17
pitot_heat = 0, 2, 17
additional_system = 0, 20, 17
marker_beacon = 1, 2, 17
gear_warning = 0, 2, 17
fuel_pump = 0, 5, 17
starter1 = 0, 20, 17
light_nav = 0, 5, 17
light_beacon = 0, 5, 17
light_landing = 0, 5, 17
light_taxi = 0, 5, 17
light_strobe = 0, 5, 17
light_panel = 0, 5, 17

[pitot_static]
vertical_speed_time_constant=1.0              //Increasing this value will cause a more instantaneous reaction in the VSI

[flight_tuning]
cruise_lift_scalar=1.0 
parasite_drag_scalar=1.0 
induced_drag_scalar=1.0 
elevator_effectiveness=1.0 
aileron_effectiveness=1.0 
rudder_effectiveness=1.0 
pitch_stability=1.0 
roll_stability=1.0 
yaw_stability=1.0 
elevator_trim_effectiveness=1.0 
aileron_trim_effectiveness=1.0 
rudder_trim_effectiveness=1.0 
hi_alpha_on_roll=-0.32306
hi_alpha_on_yaw=0.1615
p_factor_on_yaw= 1.2
torque_on_roll=1.5
gyro_precession_on_yaw=1.0
gyro_precession_on_pitch=1.0

[piston_engine] 
power_scalar=1.0                               //Piston power scalar
cylinder_displacement=81.35                    //Cubic inches per cylinder   8 litres 6 cyl
compression_ratio=8.0                          //Compression ratio
number_of_cylinders=6                          //Number of cylinders
max_rated_rpm=3300                             //Max rated RPM
max_rated_hp=300                               //Max rated HP
fuel_metering_type=0                           //0=Fuel Injected, 1=Gravity Carbureter, 2=Aerobatic Carbureter
cooling_type=1                   //BG 0        //0=Cooling type Air, 1=Cooling type Liquid
normalized_starter_torque=0.3                  //Starter torque factor
turbocharged=1                                 //Is it turbocharged? 0=FALSE, 1=TRUE
max_design_mp=48.5                             //Max design manifold pressure, (inHg)
min_design_mp=1                                //Min design manifold pressure, (inHg)
critical_altitude=4000                         //Altitude to which the turbocharger will provide max design manifold pressure (feet)
emergency_boost_type=0                         //0=None, 1=Water Injection, 2=Methanol/Water injection, 3=War Emergency Power
emergency_boost_mp_offset=0                    //Additional manifold pressure supplied by emergency boost
emergency_boost_gain_offset=0                  //Multiplier on manifold pressure due to emergency boost
fuel_air_auto_mixture=0                        //Automixture available? 0=FALSE, 1=TRUE
auto_ignition=0                                //Auto-Ignition available? 0=FALSE, 1=TRUE
max_rpm_mechanical_efficiency_scalar=1.0       //Scalar on maximum RPM mechanical efficiency
idle_rpm_mechanical_efficiency_scalar=1.0      //Scalar on idle RPM mechanical efficiency
max_rpm_friction_scalar=1.0                    //Scalar on maximum RPM friction
idle_rpm_friction_scalar=1.0                   //Scalar on idle RPM friction

[propeller]
rotation=-1
thrust_scalar=1.0                              //Propeller thrust scalar
propeller_type=0                               //0=Constant Speed, 1=Fixed Pitch
propeller_diameter=5.9                         //Propeller Diameter, (feet)
propeller_blades=2                             //Number of propeller blades
propeller_moi=8.0                              //Propeller moment of inertia
beta_max=34.5  //32                            //Maximum blade pitch angle for constant speed prop, (degrees)
beta_min=27.2  //26                            //Minimum blade pitch angle for constant speed prop, (degrees)
min_gov_rpm=1100                               //Miminum governed RPM
prop_tc=0.1                                    //Prop time-constant
gear_reduction_ratio=1.0                       //Propeller gear reduction ratio
fixed_pitch_beta=0                             //Fixed pitch angle of fixed pitch prop, (degrees)
low_speed_theory_limit=400                     //Speed at which low speed theory becomes blended in (feet/second)
prop_sync_available=0                          //Prop synchronization available? 0=FALSE, 1=TRUE
prop_deice_available=0                         //Prop de-icing available? 0=FALSE, 1=TRUE
prop_feathering_available=0                    //Prop feathering available?  0=FALSE, 1=TRUE
prop_auto_feathering_available=0               //Prop auto-feathering available?  0=FALSE, 1=TRUE
min_rpm_for_feather=0                          //Minimum RPM for prop feathering
beta_feather=90    //BG 0                             //Feathering pitch angle (degrees)
power_absorbed_cf=0.5                          //Coefficient of friction for power absorbed by propeller
defeathering_accumulators_available=0          //Defeathering accumulators available? 0=FALSE, 1=TRUE 
prop_reverse_available=0                       //Prop reverse available?  0=FALSE, 1=TRUE
minimum_on_ground_beta=0                       //Miminum pitch angle on ground, (degrees)
minimum_reverse_beta=0                         //Minimum pitch angle in reverse, (degrees)

[Views]
eyepoint=0.0, 0.0, 0.1 

[flaps.0]
type=1                                         // 1 - tail, 2 - lead
span-outboard=0.5                              // 0.0 .. 1.0
extending-time=10                              // seconds
flaps-position.0=0
flaps-position.1=5
flaps-position.2=10                            // degrees, KIAS
flaps-position.3=15
flaps-position.4=30
flaps-position.5=45                            // degrees, KIAS
flaps-position.6=60                            // degrees, KIAS
damaging-speed=250                             // KIAS
blowout-speed=300                              // KIAS
lift_scalar=1.0                                       
drag_scalar=1.0
pitch_scalar=1.0
system_type=3         //BG 0                   //0=Electric, 1=Hydraulic, 2=Pneumatic, 3=Manual, 4=None

[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, 0 
Adf.1=1 
Transponder.1=1 
Marker.1=1 

[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=1,0 

[Reference Speeds]
flaps_up_stall_speed=66.0                  //Knots True (KTAS)
full_flaps_stall_speed=52.8                //Knots True (KTAS)
cruise_speed=200                           //Knots True (KTAS)
max_indicated_speed=300

[autopilot]
autopilot_available=1 
flight_director_available=1 
default_vertical_speed=700.0 
autothrottle_available=0 
pitch_takeoff_ga=8.000000 
autoland_available=0
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

[brakes]
toe_brakes_scale=0.5
parking_brake=1

[gear_warning_system]
gear_warning_available=1
pct_throttle_limit=0.099976
flap_limit_power=15.996982
flap_limit_idle=0.000000

[hydraulic_system]
normal_pressure=60.000000                  //pression hydraulique PSI
engine_map=1,0,0,0

[stall_warning]
type=0
[attitude_indicators]
attitude_indicator.0=1
[turn_indicators]
turn_indicator.0=1,0

[exits]
number_of_exits = 2
exit_rate.0 = 0.4
exit_rate.1 = 0.4