[fltsim.0]
title=MC205_N1
sim=MC205_N1
model=N1
panel=
sound=
texture= 
kb_checklists=

ui_manufacturer=Macchi Castoldi
ui_type= MC205 "Orione"
ui_variation=N1
description=High-altitude interceptor fighter prototype. Armed with four 12.7 mm (0.5 in) machine guns mounted in the fuselage, and one 20 mm cannon mounted in the engine.\nDerived from the MC205 "Veltro", had a new wing with an increased wing aerea and new forward fuselage.\nThis made the shape in general much slimmer, instead of being a "big nose" design.\nAlso the fuselage was finally adapted for a 20 mm MG 151 cannon.
 
[fltsim.1]
title= MC205_N2
sim= MC205_N2
model=
panel=
sound=
texture=
kb_checklists=

ui_manufacturer=Macchi Castoldi
ui_type= MC205 "Orione"
ui_variation=N2
description=Derived from the MC205 N1, had no blisters on the engine cowling and on the wings\nDifferent armament:three cannons 20 mm,one in the engine and two in the wings, and two machine guns in teh engine cowling


 

[WEIGHT_AND_BALANCE]
empty_weight = 6331

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

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






[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=1350.000000
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=3
exit_rate.0=0.4	 				;Percent per second
exit_rate.1=0.4	 
exit_rate.2=0.4	 






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






[contact_points]
//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
//14 Airspeed limit for retraction (KIAS)
//15 Airspeed that gear gets damage at (KIAS)
point.0=1.0,-13.416667, 0.0,     -2.85,   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,-6.40,   2165.354400,1.0,0.557255,0.0,0.965931,2.50,0.649925,5.50,5.0,2.0,0.0,0.0
point.2=1.0,  3.250,    5.916667,-6.40,   2165.354400,2.0,0.557255,0.0,0.965931,2.50,0.649925,5.50,5.0,3.0,0.0,0.0
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







[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=-2.25,0.00,2.40






[LIGHTS]
light.0=4,0.3,0.0,2.22, fx_vclight_s403





[General]
performance=Lenth 9,65m\nWingspan 11,25 m\nEmpty weight 2,581Kg\nPower plant: 1× Fiat R.A 1050 Tifone (license-built Daimler-Benz DB 605A-1) liquid-cooled inverted V-12, 1,085 kW (1,475 hp)\nMax speed:640 km/h\nrange:950 km\nService ceiling 11,500





[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=2.000000
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=407.000000





[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