[fltsim.0]
title=Fiat_G-55_Centauro 
sim=Fiat_G-55_Centauro
model=
panel=
sound=
texture=
ui_manufacturer=Fiat
ui_type=G55 Centauro
ui_variation=Default
kb_checklists=
description=The Fiat G55 Centauro was a single engine single seat WW2 Fighter used by the Italian Air Force from 1943-1945.\nThe first prototype flew on April 30, 1942. Around 130 Centauro were produced, most of them seeing service with the Aeronautica Nazionale Repubblicana in northern Italy. After suffering repeated bombing attacks on the Turin Fiat's production plant in northern Italy, supplies of the Fiat G.55 dwindled and eventually all Italian fighter squadrons in Italy were intended to be equipped with the Me 109G. Italian pilots however tended to avoid the substitution of the G55 with a plane that they consider inferior. For this, the production of G55 and spare parts never ceased and, when the allies reached Fiat factory, they found 19 planes ready to be delivered and spare parts to build several others.\n\n

[fltsim.1]
title=Fiat_G-55_Centauro_1 
sim=Fiat_G-55_Centauro
model=
panel=2
sound=
texture=
ui_manufacturer=Fiat
ui_type=G55 Centauro
ui_variation=High view Panel
kb_checklists=
description=The Fiat G55 Centauro was a single engine single seat WW2 Fighter used by the Italian Air Force from 1943-1945.\nThe first prototype flew on April 30, 1942. Around 130 Centauro were produced, most of them seeing service with the Aeronautica Nazionale Repubblicana in northern Italy. After suffering repeated bombing attacks on the Turin Fiat's production plant in northern Italy, supplies of the Fiat G.55 dwindled and eventually all Italian fighter squadrons in Italy were intended to be equipped with the Me 109G. Italian pilots however tended to avoid the substitution of the G55 with a plane that they consider inferior. For this, the production of G55 and spare parts never ceased and, when the allies reached Fiat factory, they found 19 planes ready to be delivered and spare parts to build several others.\n\n
 
[General]
atc_type=FIAT
atc_model=G55
editable=0
performance=Length: 30'9" (9.37 m)\nWingspan: 38'10" (11.85 m)\nHeight: 10'3 1/4" (3.13 m)\nWing area: 227.23 ft² (21.11 m²)\nEmpty weight: 5,798 lb (2,630 kg)\nMaximum Take-Off Weight: 8,179 lb (3,718 kg)\nPowerplant: 1× Fiat R.A 1050 Tifone (license-built Daimler-Benz DB 605A-1) liquid-cooled inverted V-12, 1,475 hp (1,085 kW)\nMaximum speed: 385 mph (620 km/h)\nRange: 746 miles (1,160 km)\nService ceiling: 42,650 (ft12,700 m)\nArmament: 3x20 mm Mg 151/20 cannons, one engine-mounted and two wing-mounted 4x12.7 mm Breda-SAFAT machine guns Provision for two 160 kg (353 lb) bombs on underwing racks.\n\n


reference_datum_position=0.0, 0.0, 0.0	// (feet) distance from FlightSim Reference position: (1/4 chord, centerline, waterline)
empty_weight_CG_position=0.095, 0, 0       // (feet) longitudinal, lateral, vertical distance from specified datum
max_number_of_stations=10

[pitot_static]
vertical_speed_time_constant = 1


[WEIGHT_AND_BALANCE]
max_gross_weight = 8179
empty_weight = 5798          

station_load.0=200,  -3.0, 0.0, 3.0		//Pilot           Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)

;Moments of Inertia
empty_weight_pitch_MOI  = 6193
empty_weight_roll_MOI  = 5511
empty_weight_yaw_MOI  = 10832
empty_weight_coupled_MOI=0.000000
max_gross_weight=9796.500000
reference_datum_position=0.000000,0.000000,0.000000
empty_weight_CG_position=0.000000,0.000000,0.000000

[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

[piston_engine]
power_scalar=1.0
cylinder_displacement=181.500000
compression_ratio=8.500000
number_of_cylinders=12
max_rated_rpm=2800.000000
max_rated_hp=1400.000000
fuel_metering_type=0
cooling_type=1
normalized_starter_torque=0.035000
turbocharged=1
max_design_mp=39.869999
min_design_mp=9.000000
critical_altitude=22966.000000
emergency_boost_type=2
emergency_boost_mp_offset=2.210000
emergency_boost_gain_offset=0.185178
fuel_air_auto_mixture=0
auto_ignition=0
max_rpm_mechanical_efficiency_scalar=1.000000
idle_rpm_mechanical_efficiency_scalar=1.000000
max_rpm_friction_scalar=1.000000
idle_rpm_friction_scalar=1.000000

[propeller]
thrust_scalar=1.0
propeller_type=0
propeller_diameter=11.000000
propeller_blades=2
propeller_moi=27.580348
beta_max=65.000000
beta_min=15.000000
min_gov_rpm=420.000000
prop_tc=0.010000
gear_reduction_ratio=2.000000
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=70.000000
beta_feather=88.500000
power_absorbed_cf=0.900000
defeathering_accumulators_available=0
prop_reverse_available=0.000000
minimum_on_ground_beta=1.000000
minimum_reverse_beta=-14.000000

[exits]
number_of_exits=1
exit_rate.0=0.4	 				;Percent per second

[electrical]
max_battery_voltage=24.0
generator_alternator_voltage=28.0
max_generator_alternator_amps=60.0

[contact_points]
point.0=1.0,-13.416667, 0.0,     -2.40,   2165.354400,0.0,0.557255,12.0,0.292829,2.50,0.462118,3.0,3.0,0.0,0.0,0.0
point.1=1.0,  3.250,   -5.916667,-6.70,   2165.354400,1.0,0.557255,0.0,0.965931,2.50,0.649925,5.50,6.50,2.0,0.0,0.0
point.2=1.0,  3.250,    5.916667,-6.70,   2165.354400,2.0,0.557255,0.0,0.965931,2.50,0.649925,5.50,8.0,3.0,0.0,0.0
point.3=2.0,  0.0,    -18.50,     0.0,    1181.102400,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,5.0,0.0,0.0
point.4=2.0,  0.0,     18.50,     0.0,    1181.102400,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,6.0,0.0,0.0
point.5=2.0,-14.166667,0.0,      -0.50,   1181.102400,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,9.0,0.0,0.0
point.6=2.0,  9.250,   0.0,      -1.916667,1181.102400,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,4.0,0.0,0.0

static_pitch=12.0
static_cg_height=4.8
gear_system_type=1

[folding_wings]
wing_fold_system_type = 4			;0=None
fold_rates = 0.22,0.21				;Percent per second

[TailHook]
tailhook_length=4				;(feet)
tailhook_position = -17.5, 0.0, -0.5		;(feet) longitudinal, lateral, vertical positions from datum
cable_force_adjust = 1.0

[forcefeedback]
gear_bump_nose_magnitude=6000		; 0 - 10000
gear_bump_nose_direction=18000		; 0 - 35999 degrees
gear_bump_nose_duration=250000		; in microseconds
gear_bump_left_magnitude=6000		; 0 - 10000
gear_bump_left_direction=35500		; 0 - 35999 degrees
gear_bump_left_duration=250000		; in microseconds
gear_bump_right_magnitude=6000		; 0 - 10000
gear_bump_right_direction=00500		; 0 - 35999 degrees
gear_bump_right_duration=250000		; in microseconds
ground_bumps_magnitude1=3250		; 0 - 10000
ground_bumps_angle1=8900		; 0 - 35999 degrees
ground_bumps_intercept1=5.0
ground_bumps_slope1=0.48
ground_bumps_magnitude2=750		; 0 - 10000
ground_bumps_angle2=9100		; 0 - 35999 degrees
ground_bumps_intercept2=0.075
ground_bumps_slope2=1.0
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

[Views]
eyepoint=-2.9,0.0,2.5

[LIGHTS]
panel=0.00, 0.65, -0.50, fx_vclight
[General]
performance=Weight: 6531 lbs\nPower: 1350 hp\n7.5g Corner speed: 242 mph\nMax speed @ SL: 331 mph\nMax speed: 391 mph @ 22966 ft\nClimb rate: 4000 ft\/min @ 141 mph\nFlight Model By: Jerry Beckwith                       Visual model By: Ignacio Alfredo Mendive\n\n
[fuel]
Center1=0.010000,0.000000,0.000000,65.000000,0.000000
LeftMain=0.000000,-4.000000,-2.000000,25.000000,0.000000
RightMain=0.000000,4.000000,-2.000000,25.000000,0.000000
fuel_type=1.000000
number_of_tank_selectors=1
electric_pump=1
[airplane_geometry]
wing_area=227.000000
wing_span=38.916667
wing_root_chord=5.833333
wing_dihedral=4.998779
wing_incidence=0.999756
wing_twist=0.000000
oswald_efficiency_factor=0.889527
wing_winglets_flag=0
wing_sweep=0.000000
wing_pos_apex_lon=0.000000
wing_pos_apex_vert=0.000000
htail_area=27.000000
htail_span=15.583333
htail_pos_lon=-16.916667
htail_pos_vert=0.000000
htail_incidence=0.000000
htail_sweep=0.000000
vtail_area=13.000000
vtail_span=4.110961
vtail_sweep=0.000000
vtail_pos_lon=-16.916667
vtail_pos_vert=5.833333
elevator_area=18.100000
aileron_area=21.900000
rudder_area=9.800000
elevator_up_limit=30.000000
elevator_down_limit=20.000000
aileron_up_limit=15.000000
aileron_down_limit=15.000000
rudder_limit=30.000000
elevator_trim_limit=18.000000
spoiler_limit=0.000000
spoilerons_available=0
aileron_to_spoileron_gain=0.000000
min_ailerons_for_spoilerons=0.000000
min_flaps_for_spoilerons=0.000000
[brakes]
toe_brakes_scale=0.640889
parking_brake=1
[gear_warning_system]
gear_warning_available=0
pct_throttle_limit=0.000000
flap_limit_power=0.000000
flap_limit_idle=0.000000
[Flaps.0]
type=1
span-outboard=0.500000
extending-time=5.000000
system_type=1
flaps-position.0=0.000000,0.000000
flaps-position.1=15.000000,0.000000
flaps-position.2=30.000000,0.000000
flaps-position.3=45.000000,0.000000
[GeneralEngineData]
engine_type=0
Engine.0=9.250000,0.000000,-0.083333
fuel_flow_scalar=1.000000
min_throttle_limit=0.000000
[Reference Speeds]
flaps_up_stall_speed=97.000000
full_flaps_stall_speed=77.600000
cruise_speed=250.000000
max_indicated_speed=484.000000
[keyboard_response]
elevator=350.000000,500.000000
aileron=450.000000,1000.000000
rudder=200.000000,1000.000000
[autopilot]
autopilot_available=1
flight_director_available=0
default_vertical_speed=700.000000
autothrottle_available=1
autothrottle_arming_required=0
autothrottle_takeoff_ga=0
autothrottle_max_rpm=90.000000
pitch_takeoff_ga=8.000000
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
[hydraulic_system]
electric_pumps=0
engine_map=1,0,0,0
normal_pressure=6.930556
[stall_warning]
type=1
[attitude_indicators]
attitude_indicator.0=1
[turn_indicators]
turn_indicator.0=1,0
[direction_indicators]
direction_indicator.0=1,0
[WEIGHT_AND_BALANCE]
reference_datum_position=0.000000,0.000000,0.000000
empty_weight_CG_position=0.000000,0.000000,0.000000
empty_weight=6331.000000
empty_weight_roll_MOI=5511.000000
empty_weight_pitch_MOI=6193.000000
empty_weight_yaw_MOI=10832.000000
empty_weight_coupled_MOI=0.000000
max_gross_weight=9496.500000