[fltsim.0]
title=ME109_G
sim=ME109_G
model=
panel=
sound=
texture=
ui_manufacturer=MESSERSCHMITT
ui_type=ME109_G
ui_variation=Gustav
kb_checklists=
description=Notes:The German Messerschmitt based his design on the experiance he had gained with the Bf 108. It was an excellent lightweight plane, which was superior to the modern fighter planes used by some nations at that time. So Messerschmitt optimized the fuselage, reduced the weight and fitted this design with the most powerful engine available at that time.

[fltsim.1]
title=ME109_GPaint1
sim=ME109_G
model=
panel=
sound= 
ui_manufacturer=MESSERSCHMITT
ui_type= ME109_G_ ANR
ui_variation=Gustav  ANR
texture=1
kb_checklists=
description=Notes:The German Messerschmitt based his design on the experiance he had gained with the Bf 108. It was an excellent lightweight plane, which was superior to the modern fighter planes used by some nations at that time. So Messerschmitt optimized the fuselage, reduced the weight and fitted this design with the most powerful engine available at that time.
atc_heavy=0
atc_id=1769
atc_airline=one 4
atc_flight_number=xgust

[WEIGHT_AND_BALANCE]
performance=Length:8.94m\nWing span:9.92m\nWeight:MTOW 3200 kg\n Empty 2709 kg\nPower:1xDaimler Benz 605A1,475Hp\nDetails:\nDesigners:ItaloD'Attomo and Giovanni Quai\nDate:November 2005\n\n
reference_datum_position=0.000000,0.000000,0.000000
empty_weight_CG_position=0.000000,0.000000,0.000000
empty_weight=6285.000000
empty_weight_roll_MOI=14097.000000
empty_weight_pitch_MOI=10138.000000
empty_weight_yaw_MOI=20372.000000
empty_weight_coupled_MOI=0.000000
max_gross_weight=7054.000000

[flight_tuning]
cruise_lift_scalar = 1
parasite_drag_scalar = 0.6
induced_drag_scalar = 1.4
elevator_effectiveness = 1
aileron_effectiveness = 1.5
rudder_effectiveness = 1
pitch_stability = 1
roll_stability = 1
yaw_stability = 1
elevator_trim_effectiveness = 1.3
aileron_trim_effectiveness = 1
rudder_trim_effectiveness = 1

[piston_engine]
power_scalar = 1
cylinder_displacement = 148.888888888889
compression_ratio = 8
number_of_cylinders = 12
max_rated_rpm = 3000
max_rated_hp = 1775
fuel_metering_type = 1
cooling_type = 1
normalized_starter_torque = 0.07
turbocharged = 1
max_design_mp = 54
min_design_mp = 9
critical_altitude = 5100
emergency_boost_type = 0
emergency_boost_mp_offset = 0
emergency_boost_gain_offset = 0
fuel_air_auto_mixture = 0
auto_ignition = 0
max_rpm_mechanical_efficiency_scalar = 1
idle_rpm_mechanical_efficiency_scalar = 1
max_rpm_friction_scalar = 1
idle_rpm_friction_scalar = 1

[propeller]
thrust_scalar = 1
propeller_type = 0
propeller_diameter = 9
propeller_blades = 3
propeller_moi = 14.1
beta_max = 65
beta_min = 15
min_gov_rpm = 337.5
prop_tc = 0.01
gear_reduction_ratio = 1
fixed_pitch_beta = 30
low_speed_theory_limit = 80
prop_sync_available = 0
prop_deice_available = 0
prop_feathering_available = 0
prop_auto_feathering_available = 0
min_rpm_for_feather = 700
beta_feather = 88.5
power_absorbed_cf = 0.9
defeathering_accumulators_available = 0
prop_reverse_available = 0
minimum_on_ground_beta = 1
minimum_reverse_beta = -14
rotation = 1

[contact_points]
max_number_of_points = 9
point.0 = 1, -16.2, 0, -2.1, 1600, 0, 0.531197, 41.64, 0.551117, 2.5, 0.686607, 5, 5, 0, 0, 0
point.1 = 1, 4.3, -4, -6.1, 1600, 1, 0.531197, 0, 0.714684, 2.5, 0.274063, 4.1, 4.1, 2, 0, 0
point.2 = 1, 4.3, 4, -6.1, 1600, 2, 0.531197, 0, 0.714684, 2.5, 0.274063, 8.2, 8.2, 3, 0, 0
point.3 = 2, -1, -21.6, 0.2, 1600, 0, 0, 0, 0, 0, 0, 0, 0, 5
point.4 = 2, -1, 21.6, 0.2, 1600, 0, 0, 0, 0, 0, 0, 0, 0, 6
point.5 = 2, -19.4, 0, 0.9, 1600, 0, 0, 0, 0, 0, 0, 0, 0, 9
point.6 = 2, 0, 0, -2.2, 1600, 0, 0, 0, 0, 0, 0, 0, 0, 4
point.7 = 2, 10, 0, 0.2, 1600, 0, 0, 0, 0, 0, 0, 0, 0, 4
point.8 = 2, 9.8, 0, -4, 1600, 0, 0, 0, 0, 0, 0, 0, 0, 4

static_pitch= 12
static_cg_height= 4.90927
gear_system_type=1


[Views]
eyepoint= -0.2, 0, 3.35

[flaps.0]       //Trailing Edge Flaps
type = 1
span-outboard = 0.5
extending-time = 5
flaps-position.0 = 0
flaps-position.1 =10
flaps-position.2 = 16
flaps-position.3 = 25
flaps-position.4 = 35
damaging-speed = 145
blowout-speed = 125

[Flaps.1]
type=2
span-outboard=0.5
extending-time=5.
system_type=0
flaps-position.0=0.
flaps-position.1=100

[electrical]
max_battery_voltage = 24
generator_alternator_voltage = 28
max_generator_alternator_amps = 160
electric_always_available = 1

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
starter2 = 0, 20, 17
starter3 = 0, 20, 17
starter4 = 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
prop_sync = 0, 15, 17
auto_feather = 0, 15, 17
auto_brakes = 0, 15, 17
standby_vacuum = 0, 15, 17
hydraulic_pump = 0, 2, 17
fuel_transfer_pump = 0, 5, 17
propeller_deice = 0, 5, 17
light_recognition = 0, 5, 17
light_wing = 0, 5, 17
light_logo = 0, 5, 17

[LIGHTS]
//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit            
light.0=3,  5.70, -16.40, 0.16, fx_navred
light.1=3,  5.70, 16.40, 0.16, fx_navgre
panel = 0, 0.35, -0.8, fx_vclight


[LSO]
LSOAdjustSpeed = 1.2

[exits]
number_of_exits = 1
exit_rate.0 = 0.4


[General]
performance=Max Weight 7054 lbs\n Power: 1475 hp\nMax speed @ SL: 326 mph (525Kmh)\n Max speed@ 7000 mt: 403 mph(650 kmh) \n

[fuel]
LeftMain=0.000000,-2.500000,0.000000,55.500000,0.000000
RightMain=0.000000,2.500000,0.000000,55.500000,0.000000
fuel_type=1.000000
number_of_tank_selectors=1
electric_pump=1

[airplane_geometry]
wing_area=254.000000
wing_span=42.000000
wing_root_chord=7.500000
wing_dihedral=5.597534
wing_incidence=0.000000
wing_twist=0.000000
oswald_efficiency_factor=0.891323
wing_winglets_flag=0
wing_sweep=0.000000
wing_pos_apex_lon=1.510119
wing_pos_apex_vert=0.000000
htail_area=34.000000
htail_span=13.000000
htail_pos_lon=-17.916667
htail_pos_vert=0.000000
htail_incidence=0.000000
htail_sweep=0.000000
vtail_area=19.000000
vtail_span=4.969909
vtail_sweep=0.000000
vtail_pos_lon=-19.500000
vtail_pos_vert=7.250000
elevator_area=26.600000
aileron_area=18.900000
rudder_area=14.900000
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=0.885
parking_brake=1

[gear_warning_system]
gear_warning_available=0
pct_throttle_limit=0.099976
flap_limit_power=33.750000
flap_limit_idle=16.875000

[GeneralEngineData]
engine_type=0
Engine.0=9.750000,0.000000,0.000000
fuel_flow_scalar=1.000000
min_throttle_limit=0.000000

[Reference Speeds]
flaps_up_stall_speed=73
full_flaps_stall_speed=58
cruise_speed=250
max_indicated_speed=503

[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=0
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