[fltsim.0]
title=Me329
sim=Me_329
model=
panel=
sound=
texture=
kb_reference=Me_329_ref
KB_checklists=Me_329_check
description=The Me329 was originally designed in 1942 but never came into production. Only a wood mockup was ever built and the Me329 was not pursued due to development time. Plus the Me410 was proving to be a much more hopefull design. The Me329 would have had a 2 man crew. The craft would have been armed with four MG 151\/20 20mm cannons mounted in the nose and two MK 103 30mm cannons in the wing roots. The rear cannon was operated by the second crew member via a periscope system. The Me329 intended role would have been a heavy fighter\/bomber and would have been capable of carrying 2400Kg of bombs. This version of the Me329 is a single seat Aero Racer done in imaginary colours, equiped with a smoke display system, and modern cockpit instruments.
ui_manufacturer=Messerschmitt
ui_type=Me 329
ui_variation=Danger Girl Aero Racer
atc_heavy=0
atc_id=M000EX
atc_airline=
atc_flight_number=

[WEIGHT_AND_BALANCE]
empty_weight= 12264.000

reference_datum_position= -3.000, 0.000, 0.000
empty_weight_CG_position= 0.000, 0.000, 0.000

max_number_of_stations=50

station_load.0= 170.000, -3.000, 0.000, 3.000

;Moments of Inertia
empty_weight_pitch_MOI= 19696.000
empty_weight_roll_MOI= 16104.000
empty_weight_yaw_MOI= 29242.000
empty_weight_coupled_MOI= 0.000
max_gross_weight= 17919.000
CG_forward_limit= 0.000
CG_aft_limit= 1.000


[flight_tuning]
cruise_lift_scalar=1.000
parasite_drag_scalar=1.000
induced_drag_scalar=1.000
elevator_effectiveness=1.500
aileron_effectiveness=1.500
rudder_effectiveness=1.500
pitch_stability=1.000
roll_stability=1.000
yaw_stability=1.000
elevator_trim_effectiveness=1.000
aileron_trim_effectiveness=1.000
rudder_trim_effectiveness=1.000

[piston_engine]
power_scalar=1.000
cylinder_displacement= 226.000
compression_ratio= 7.000
number_of_cylinders= 12
max_rated_rpm= 3000.000
max_rated_hp= 2700.000
fuel_metering_type= 0
cooling_type= 1
normalized_starter_torque= 0.035
turbocharged= 1
max_design_mp= 54.000
min_design_mp= 1.000
critical_altitude= 21000.000
emergency_boost_type= 0
emergency_boost_mp_offset= 0.000
emergency_boost_gain_offset= 0.000
fuel_air_auto_mixture= 0
auto_ignition= 0
max_rpm_mechanical_efficiency_scalar=1.000
idle_rpm_mechanical_efficiency_scalar=1.000
max_rpm_friction_scalar=1.000
idle_rpm_friction_scalar=1.000

[propeller]
thrust_scalar=1.500
rotation=-1,1		//Engine 1,2,3,... Rotation direction. 1 = CW, -1 = CCW
propeller_type= 0
propeller_diameter= 14.000
propeller_blades= 3
propeller_moi= 72.000
beta_max= 65.000
beta_min= 23.000
min_gov_rpm= 1800.000
prop_tc= 0.010
gear_reduction_ratio= 2.237
fixed_pitch_beta= 0.000
low_speed_theory_limit= 80.000
prop_sync_available= 0
prop_deice_available= 0
prop_feathering_available= 0
prop_auto_feathering_available= 0
min_rpm_for_feather= 0.000
beta_feather= 0.000
power_absorbed_cf= 0.000
defeathering_accumulators_available= 0
prop_reverse_available= 0
minimum_on_ground_beta= 0.000
minimum_reverse_beta= 0.000

[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]
//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= 1.000, 16.960, 0.000, -7.470, 1600.000, 0.000, 1.250, 37.700, 0.400, 2.500, 0.950, 2.500, 3.000, 0.000, 0.000, 0.000
point.1= 1.000, -1.140, -8.230, -7.470, 2200.000, 1.000, 1.670, 0.000, 0.400, 2.500, 0.750, 5.500, 5.000, 2.000, 0.000, 0.000
point.2= 1.000, -1.140, 8.230, -7.470, 2200.000, 2.000, 1.670, 0.000, 0.400, 2.500, 0.750, 6.500, 5.000, 3.000, 0.000, 0.000
point.3= 2.000, -3.530, -28.560, 0.140, 1200.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 5.000, 0.000, 0.000
point.4= 2.000, -3.530, 28.560, 0.140, 1200.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 6.000, 0.000, 0.000
point.5= 2.000, -4.200, 0.000, -5.920, 1200.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 9.000, 0.000, 0.000
point.6= 2.000, 9.140, 0.000, -2.770, 1200.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 4.000, 0.000, 0.000

static_cg_height= 7.070
static_pitch= 0.000

[Views]
eyepoint=3.00,0.000000,0.000000

[SMOKESYSTEM]
smoke.0=-8.50, 0.00, 0.00, fx_smoke_r

[LIGHTS]
//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit        
light.0=3,  -3.55, -28.62, 0.14, fx_navred
light.1=3,  -3.55,  28.62, 0.14, fx_navgre
light.2=2,   9.15,   0.00,-2.78, fx_strobe
light.3=1,  -7.16,   0.00, 8.49, fx_beacon
light.4=4,  15.00,   0.00, 1.20, fx_vclight

[General]
performance=Weight: 15,322\/ 26,786 lbs\nEngines:2  Daimler Benz ( now Mercedes Benz )\nDB603L inverted V12 45lt engines with Hirth supercharges, each producing 2100hp.\nMax speed: +400 mph @ 25,000 ft.\nCeiling: 39,000 ft.\nInitial climb rate: 2,500 ft\/min.\nRange: approx  1,750 miles.\nWing span: 57.5 ft\nLenght: 25.3 ft\nHeight: 15.5 ft
atc_type=EXPERIMENTAL
atc_model=EXPL

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

[fuel]
Center1= 0.000, 0.000, 0.000, 180.000, 0.000
LeftMain= 0.000, 0.000, 0.000, 135.000, 0.000
RightMain= 0.000, 0.000, 0.000, 135.000, 0.000
External1= 0.000, 0.000, 0.000, 225.000, 0.000
External2= 0.000, 0.000, 0.000, 225.000, 0.000
fuel_type=1.000000
number_of_tank_selectors=1

[airplane_geometry]
wing_area= 358.000
wing_span= 52.000
wing_root_chord= 6.917
wing_dihedral= 5.098
wing_incidence= 1.000
wing_twist= 0.000
oswald_efficiency_factor= 0.749
wing_winglets_flag= 0
wing_sweep= 0.000
wing_pos_apex_lon= 2.000
wing_pos_apex_vert= 0.000
htail_area= 34.000
htail_span= 10.500
htail_pos_lon= -17.667
htail_pos_vert= 0.000
htail_incidence= 0.000
htail_sweep= 0.000
vtail_area= 15.000
vtail_span= 4.416
vtail_sweep= 0.000
vtail_pos_lon= -19.583
vtail_pos_vert= 3.250
elevator_area= 13.260
aileron_area= 18.900
rudder_area= 8.230
elevator_up_limit= 28.000
elevator_down_limit= 22.999
aileron_up_limit= 26.001
aileron_down_limit= 18.999
rudder_limit= 28.000
elevator_trim_limit= 19.996
spoiler_limit= 0.000
spoilerons_available= 0
aileron_to_spoileron_gain= 0.000
min_ailerons_for_spoilerons= 0.000
min_flaps_for_spoilerons= 0.000

[GeneralEngineData]
engine_type= 0
Engine.0= 1.000, -8.235, 1.400
Engine.1= -1.000, 8.235, 1.400
fuel_flow_scalar= 1.000

[Reference Speeds]
flaps_up_stall_speed= 64.000
full_flaps_stall_speed= 51.200
cruise_speed= 284.532

[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

[direction_indicators]
direction_indicator.0=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

[Flaps.0]
type= 1
span-outboard= 0.125
extending-time= 5.000
system_type= 0
damaging-speed= 191.000
blowout-speed= 290.000
lift_scalar= 0.500
drag_scalar= 1.500
pitch_scalar= 1.000
flaps-position.0= 0.000, 0.000
flaps-position.1= 12.500, 0.000
flaps-position.2= 25.000, 0.000