[fltsim.0]
title=Messerschmitt Bf 109G4 Hart
sim=Bf109G4_10
model=bf109g4_10

[General]
editable=0

[WEIGHT_AND_BALANCE]
max_gross_weight=7946.00
empty_weight=5880.00

reference_datum_position=8.90,0.00,0.00
empty_weight_CG_position=-8.90,0.00,0.00

max_number_of_stations=50
station_load.0=180.00,-12.40,0.00,0.00

empty_weight_roll_MOI=3129.00
empty_weight_pitch_MOI=5125.00
empty_weight_yaw_MOI=6563.00
empty_weight_coupled_MOI=0.00

CG_forward_limit=0.00
CG_aft_limit=1.00

[fuel]
Center1=-15.90,0.00,-1.00,105.00,0.00
fuel_type= 1.000
number_of_tank_selectors= 1

[airplane_geometry]
wing_area=173.00
wing_span=32.58
wing_root_chord=7.20
wing_dihedral=8.00
wing_incidence=1.70
wing_twist=0.00
oswald_efficiency_factor=0.70
wing_winglets_flag=0
wing_sweep=5.00
wing_pos_apex_lon=-6.90
wing_pos_apex_vert=-1.10
htail_area=28.00
htail_span=9.60
htail_pos_lon=-25.00
htail_pos_vert=2.00
htail_incidence=-0.50
htail_sweep=10.00
vtail_area=25.00
vtail_span=4.10
vtail_sweep=32.00
vtail_pos_lon=-25.00
vtail_pos_vert=1.60
elevator_area=19.00
aileron_area=19.00
rudder_area=19.00
elevator_up_limit=34.00
elevator_down_limit=34.00
aileron_up_limit=17.00
aileron_down_limit=12.00
rudder_limit=40.00
elevator_trim_limit=12.00
spoiler_limit=0.00
spoilerons_available=0
aileron_to_spoileron_gain=0.00
min_ailerons_for_spoilerons=0.00
min_flaps_for_spoilerons=0.00

[Flaps.0]
type=1
span-outboard=0.50
extending-time=3.00
system_type=3
damaging-speed=135.00
blowout-speed=150.00
lift_scalar=1.00
drag_scalar=1.00
pitch_scalar=1.00
flaps-position.0=0.00
flaps-position.1=10.50
flaps-position.2=20.00
flaps-position.3=31.50
flaps-position.4=42.00

[Reference Speeds]
flaps_up_stall_speed=91.00
full_flaps_stall_speed=72.80
cruise_speed=208.0

[flight_tuning]
cruise_lift_scalar=1.00
pitch_stability=1.00
roll_stability=1.00
yaw_stability=1.00
parasite_drag_scalar=1.00
induced_drag_scalar=1.00
elevator_effectiveness=1.00
aileron_effectiveness=1.00
rudder_effectiveness=1.00
elevator_trim_effectiveness=1.00
aileron_trim_effectiveness=1.00
rudder_trim_effectiveness=1.00

[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=1.00,-26.40,0.00,-1.5,2165.354,0.00,0.57,180.00,0.3,2.50,0.563,3.00,3.00,0.00,190.00,200.00
point.1=1.00,-6.90,-3.40,-5.75,2165.354,1.00,1.10,0.00,0.45,2.50,0.501,6.50,6.50,2.00,190.00,200.00
point.2=1.00,-6.90,3.40,-5.75,2165.354,2.00,1.10,0.00,0.45,2.50,0.501,9.00,9.00,3.00,190.00,200.00
point.3=2.00,0.00,0.00,0.00,2100.0,0.00,0.00,0.00,0.00,0.00,0.00,0.00,0.00,4.00,0.00,0.00
point.4=2.00,-10.20,0.00,-2.00,3000.10,0.00,0.00,0.00,0.00,0.00,0.00,0.00,0.00,4.00,0.00,0.00
point.5=2.00,-9.30,-16.10,0.40,800.10,0.00,0.00,0.00,0.00,0.00,0.00,0.00,0.00,5.00,0.00,0.00
point.6=2.00,-9.30,16.10,0.40,800.10,0.00,0.00,0.00,0.00,0.00,0.00,0.00,0.00,6.00,0.00,0.00
point.7=2.00,-27.60,0.00,5.76,700.10,0.00,0.00,0.00,0.00,0.00,0.00,0.00,0.00,9.00,0.00,0.00
point.8=2.00,-1.5,0.00,-4.00,650.0,0.00,0.00,0.00,0.00,0.00,0.00,0.00,0.00,4.00,0.00,0.00
point.9=2.00,-27.5,0.00,1.2,1200.0,0.00,0.00,0.00,0.00,0.00,0.00,0.00,0.00,4.00,0.00,0.00
point.10=2.00,-9.30,-8.10,0.40,1000.0,0.00,0.00,0.00,0.00,0.00,0.00,0.00,0.00,5.00,0.00,0.00
point.11=2.00,-9.30,8.10,0.40,1000.0,0.00,0.00,0.00,0.00,0.00,0.00,0.00,0.00,6.00,0.00,0.00

static_pitch=13.26
static_cg_height=4.87
tailwheel_lock = 1

[GeneralEngineData]
engine_type=0
Engine.0=-1.5,0.00,0.00

[piston_engine]
cylinder_displacement=190.00
compression_ratio=7.50
number_of_cylinders=12
max_rated_rpm=2800.00
max_rated_hp=1550.00
fuel_metering_type=0
cooling_type=1
normalized_starter_torque=0.035
turbocharged=1
max_design_mp=42.5
min_design_mp=1.00
critical_altitude=24250.00
emergency_boost_type=2
emergency_boost_mp_offset=4.00
emergency_boost_gain_offset=0.367
emergency_boost_duration = 600
fuel_air_auto_mixture=1
auto_ignition=0
max_rpm_mechanical_efficiency_scalar=1.00
idle_rpm_mechanical_efficiency_scalar=1.00
max_rpm_friction_scalar=1.00
idle_rpm_friction_scalar=1.00
power_scalar=1.00
fuel_flow_scalar=1.00

[propeller]
propeller_type=0
propeller_diameter=9.833
propeller_blades=3
propeller_moi=25.00
beta_max=65.00
beta_min=23.00
min_gov_rpm=1800.00
prop_tc=0.01
gear_reduction_ratio=1.685
fixed_pitch_beta=0.00
low_speed_theory_limit=80.00
prop_sync_available=0
prop_deice_available=0
prop_feathering_available=0
prop_auto_feathering_available=0
min_rpm_for_feather=0.00
beta_feather=0.00
power_absorbed_cf=0.00
defeathering_accumulators_available=0
prop_reverse_available=0
minimum_on_ground_beta=0.00
minimum_reverse_beta=0.00
thrust_scalar=1.00

[keyboard_response]
elevator= 350.000, 500.000
aileron= 450.000, 1000.000
rudder= 200.000, 1000.000

[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