[fltsim.0]
title=BT-13 Silver
sim=BT-13
model=
panel=
sound=
texture=
kb_checklists=
prop_anim_ratio=1.76
ui_manufacturer=Vultee
ui_type=Vultee Bt-13
ui_variation=Silver
atc_id_color=0x00000000
atc_heavy=0
atc_id_font=Verdana,-11,1,600,0
visual_damage=0
description=World War 2 basic trainer, over 13,000 built.
[General]
atc_type=Vibrator
atc_model=
editable=0
performance=Length: 28' 7"\nWing span: 42'\nWeight: 2976# empty, 3991# gross\nPower:P&W Wasp Jr. rated @ 450hp.\nMax Speed:182 mph\nCruise:170 mph\nCeiling:21,000 ft.\nRange:1050 miles\nDesigner: P. Clawson\nDate: 12\/2005\n\n
[fltsim.1]
title=BT-13 Yellow Blue
sim=BT-13
model=
panel=
sound=
texture=1
kb_checklists=
prop_anim_ratio=1.76
ui_manufacturer=Vultee
ui_type=Vultee Bt-13
ui_variation=Yellow Blue
atc_id_color=0x00000000
atc_heavy=0
atc_id_font=Verdana,-11,1,600,0
visual_damage=0
description=World War 2 basic trainer, over 13,000 built.
[General]
atc_type=Vibrator
atc_model=
editable=0
performance=Length: 28' 7"\nWing span: 42'\nWeight: 2976# empty, 3991# gross\nPower:P&W Wasp Jr. rated @ 450hp.\nMax Speed:182 mph\nCruise:170 mph\nCeiling:21,000 ft.\nRange:1050 miles\nDesigner: P. Clawson\nDate: 12\/2005\n\n
[weight_and_balance]
// ACM V2.5
max_gross_weight = 3991
empty_weight = 2976
reference_datum_position = 7.24, 0, 0
empty_weight_CG_position = -7.76, 0, -1
empty_weight_pitch_MOI = 1788.8
empty_weight_roll_MOI = 1606.8
empty_weight_yaw_MOI = 3429.5
empty_weight_coupled_MOI = 0
max_number_of_stations = 2
station_load.0 = 170, -6.32, 0, 0.56
station_load.1 = "0.0, -9.0, 0.0, -0.5, Navigator"
[lights]
//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing
light.0 = 4, -6.00, 0.00, 2.20, fx_vclight,
[GeneralEngineData]
//0=Piston, 1=Jet, 2=None, 3=Helo-Turbine, 4=Rocket, 5=Turboprop
engine_type = 0
fuel_flow_scalar = 1.0
min_throttle_limit = 0.0
engine.0 = 0.34, -0.06, -0.05,
[effects]
wake = fx_wake
water = fx_spray
dirt = fx_tchdrt
concrete = fx_sparks
touchdown = fx_tchdwn_s, 1
startup = fx_engstrt_vega
windshield_rain_effect_available = 1
[fuel]
//Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)
fuel_type = 1
number_of_tank_selectors = 1
electric_pump = 0
LeftMain = -6.2, -4.2, 2.7, 96, 0
RightMain = -6.2, 4.2, 2.7, 96, 0
[contact_points]
static_pitch = 11.5
static_cg_height = 4.6
tailwheel_lock = 0
gear_system_type = 0
max_number_of_points = 7
point.0 = 1, -24.8071, 0, -2.4605, 1200, 0, 0.4, 0, 0.4, 2.5, 0.595, 0, 0, 0, 0, 0
point.1 = 1, -5.7684, -5.2872, -6.4, 1600, 1, 1.2, 0, 0.6, 2.5, 0.756, 0, 0, 2, 0, 0
point.2 = 1, -5.8336, 5.2872, -6.4, 1600, 2, 1.2, 0, 0.6, 2.5, 0.752, 0, 0, 3, 0, 0
point.3 = 2, -8, -21.09, -0.9722, 800, 0, 0, 0, 0, 0, 0, 0, 0, 5, 0, 0
point.4 = 2, -8, 21.221, -0.7753, 800, 0, 0, 0, 0, 0, 0, 0, 0, 6, 0, 0
point.5 = 2, -27.4812, 0, 0.1054, 800, 0, 0, 0, 0, 0, 0, 0, 0, 9, 0, 0
point.6 = 2, 0.4908, 0, -2.4281, 800, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0
[keyboard_response]
elevator = 200, 1000
aileron = 200, 1000
rudder = 200, 1000
[forcefeedback]
ground_bumps_magnitude1 = 2600
ground_bumps_angle1 = 8900
ground_bumps_intercept1 = 5.0
ground_bumps_slope1 = 0.6
ground_bumps_magnitude2 = 1200
ground_bumps_angle2 = 9100
ground_bumps_intercept2 = 0.085
ground_bumps_slope2 = 0.65
crash_magnitude1 = 10000
crash_direction1 = 01000
crash_magnitude2 = 10000
crash_direction2 = 9000
crash_period2 = 75000
crash_duration2 = 3500000
[airplane_geometry]
wing_area = 238.0
wing_span = 42
wing_root_chord = 7.40
wing_dihedral = 4
wing_incidence = 1.0
wing_twist = 0.0
oswald_efficiency_factor = 0.6
wing_winglets_flag = 0
wing_sweep = 2.5
wing_pos_apex_lon = -4.83
wing_pos_apex_vert = -1.99
htail_area = 51.0
htail_span = 14.09
htail_pos_lon = -21.79
htail_pos_vert = 0.18
htail_incidence = -1.0
htail_sweep = 12
vtail_area = 10.0
vtail_span = 5.59
vtail_sweep = 18
vtail_pos_lon = -20.80
vtail_pos_vert = 1.5
elevator_area = 16.3
aileron_area = 25.6
rudder_area = 18
elevator_up_limit = 22.0
elevator_down_limit = 22.0
aileron_up_limit = 22.0
aileron_down_limit = 22.0
rudder_limit = 22.0
elevator_trim_limit = 20.0
spoiler_limit = 0.0
aileron_to_spoileron_gain = 0
spoiler_handle_available = 1
min_ailerons_for_spoilerons = 0
min_flaps_for_spoilerons = 0
spoilerons_available = 0
[electrical]
max_battery_voltage = 24
generator_alternator_voltage = 25
max_generator_alternator_amps = 60
engine_generator_map = 1
electric_always_available = 0
[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
[Flaps.0]
type= 1
span-outboard= 0.5
extending-time= 4.0
system_type= 0
flaps-position.0= 0.0, 0.0
flaps-position.1= 40.0, 0.0
[piston_engine]
power_scalar=1.0 //Piston power scalar
cylinder_displacement=149.3 //Cubic inches per cylinder
compression_ratio=6.0 //Compression ratio
number_of_cylinders=9 //Number of cylinders
max_rated_rpm=2200 //Max rated RPM
max_rated_hp=450 //Max rated HP
fuel_metering_type=1 //0=Fuel Injected, 1=Gravity Carburetor, 2=Aerobatic Carburetor
cooling_type=0 //0=Cooling type Air, 1=Cooling type Liquid
normalized_starter_torque=0.3 //Starter torque factor
turbocharged=1 //Is it turbocharged? 0=FALSE, 1=TRUE
max_design_mp=34 //Max design manifold pressure, (inHg)
min_design_mp=10 //Min design manifold pressure, (inHg)
critical_altitude=9000 //Altitude to which the turbocharger will provide max design manifold pressure (feet)
emergency_boost_type=0 //0=None, 1=Water Injection, 2=Methanol/Water injection, 3=War Emergency Power
emergency_boost_mp_offset=0 //Additional manifold pressure supplied by emergency boost
emergency_boost_gain_offset=0 //Multiplier on manifold pressure due to emergency boost
fuel_air_auto_mixture=0 //Automixture available? 0=FALSE, 1=TRUE
auto_ignition=0 //Auto-Ignition available? 0=FALSE, 1=TRUE
max_rpm_mechanical_efficiency_scalar=1.0 //Scalar on maximum RPM mechanical efficiency
idle_rpm_mechanical_efficiency_scalar=1.0 //Scalar on idle RPM mechanical efficiency
max_rpm_friction_scalar=1.0 //Scalar on maximum RPM friction
idle_rpm_friction_scalar=1.0 //Scalar on idle RPM friction
[propeller]
thrust_scalar=1.0 //Propeller thrust scalar
propeller_type=0 //0=Constant Speed, 1=Fixed Pitch
propeller_diameter=9 //Propeller Diameter, (feet)
propeller_blades=2 //Number of propeller blades
propeller_moi=8.0 //Propeller moment of inertia
beta_max=24.0 //Maximum blade pitch angle for constant speed prop, (degrees)
beta_min=14.0 //Minimum blade pitch angle for constant speed prop, (degrees)
min_gov_rpm=1400 //Miminum governed RPM
prop_tc=0.1 //Prop time-constant
gear_reduction_ratio=1.0 //Propeller gear reduction ratio
fixed_pitch_beta=0 //Fixed pitch angle of fixed pitch prop, (degrees)
low_speed_theory_limit=80 //Speed at which low speed theory becomes blended in (feet/second)
prop_sync_available=0 //Prop synchronization available? 0=FALSE, 1=TRUE
prop_deice_available=0 //Prop de-icing available? 0=FALSE, 1=TRUE
prop_feathering_available=0 //Prop feathering available? 0=FALSE, 1=TRUE
prop_auto_feathering_available=0 //Prop auto-feathering available? 0=FALSE, 1=TRUE
min_rpm_for_feather=0 //Minimum RPM for prop feathering
beta_feather=0 //Feathering pitch angle (degrees)
power_absorbed_cf=0 //Coefficient of friction for power absorbed by propeller in feather
defeathering_accumulators_available=0 //Defeathering accumulators available? 0=FALSE, 1=TRUE
prop_reverse_available=0 //Prop reverse available? 0=FALSE, 1=TRUE
minimum_on_ground_beta=0 //Miminum pitch angle on ground, (degrees)
minimum_reverse_beta=0 //Minimum pitch angle in reverse, (degrees)
//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
[brakes]
parking_brake = 1 //Parking brake available
toe_brakes_scale = 0.5 //Brake scalar
differential_braking_scale = 1.0 //Delta on the amount of brake when the rudder pedals deflected
[hydraulic_system]
normal_pressure = 3000.0 //PSI
engine_map=1,0,0,0
[Views]
eyepoint=-7.25, 0, 2.75
[Radios]
// Radio Type = availiable, standby frequency, has glide slope
Audio.1=1
Com.1=1, 0
Nav.1=0, 0, 0
Adf.1=1
Transponder.1=0
Marker.1=0
[direction_indicators]
//1 Type: 0=None, 1=Vacuum Gyro, 2=Electric Gyro, 3=Electro-Mag Slaved Compass, 4=Slaved to another
//2 Indicator number of slaving indicator if Type = 4
direction_indicator.0=1,0
direction_indicator.1=2,0
[attitude_indicators]
//Type: 0=None, 1=Vacuum Gyro, 2=Electric Gyro
attitude_indicator.0 = 2
[turn_indicators]
//Type: 0=None, 1=Electric Gyro, 2= Vacuum Gyro
turn_indicator.0=2,0
[Reference Speeds]
flaps_up_stall_speed=62.5 //Knots True (KTAS)
full_flaps_stall_speed=62.5 //Knots True (KTAS)
cruise_speed=139.0 //Knots True (KTAS)
max_indicated_speed = 200 //Red line (KIAS)
[autopilot]
autopilot_available=0
flight_director_available=0
pitch_takeoff_ga=0.0
default_vertical_speed=700.000000
autothrottle_available=0
direction_indicator=1
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 = 0.0
default_bank_mode=2 //Default to Heading Hold
[stall_warning]
type=1
[exits]
number_of_exits = 2
exit_rate.0 = 0.4 ;Percent per second
exit_rate.1 = 0.4 ;Percent per second
