[fltsim.0]
title=G4M2 Betty #0
sim=G4M2_Betty
model=
panel=
sound=
texture=
ui_manufacturer=
ui_type= #0
ui_variation=
description=
[WEIGHT_AND_BALANCE]
empty_weight = 17623.00 // (pounds)
reference_datum_position = 0.0, 0, 0 // (feet) distance from FlightSim Reference position: (1/4 chord, centerline, waterline)
empty_weight_CG_position = 0.0, 0, 0 // (feet) longitudinal, lateral, vertical distance from specified datum
max_number_of_stations = 50
station_load.0 = 170, 9.8, -2.0, 3.5 //Pilot Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.1 = 170, 9.8, 2.0, 3.5 //Co-Pilot Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
;Moments of Inertia
empty_weight_pitch_MOI = 81996.92 //slug-ft^2
empty_weight_roll_MOI = 57050.95 //slug-ft^2
empty_weight_yaw_MOI = 111054.86 //slug-ft^2
empty_weight_coupled_MOI= 0.000
max_gross_weight= 28253.000
[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= 125.000
compression_ratio= 7.000
number_of_cylinders= 14
max_rated_rpm= 2600.000
max_rated_hp= 1800.000
fuel_metering_type= 0
cooling_type= 0
normalized_starter_torque= 0.035
turbocharged= 1
max_design_mp= 48.000
min_design_mp= 1.000
critical_altitude= 15000.000
emergency_boost_type= 1
emergency_boost_mp_offset= 4.000
emergency_boost_gain_offset= 0.528
fuel_air_auto_mixture= 0
auto_ignition= 0
fuel_flow_scalar= 1.000
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 = 1.0
propeller_type= 0
propeller_diameter= 11.300
propeller_blades= 4
propeller_moi= 50.500
beta_max= 50.000
beta_min= 20.000
min_gov_rpm= 1700.000
prop_tc= 0.010
gear_reduction_ratio= 1.750
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
point.0=1, -32.00, 0.00, -5.85, 1600, 0, 0.90, 75.0, 0.60, 2.5, 0.80, 6.0, 6.0, 0
point.1=1, 1.74, -10.00, -9.30, 2200, 1, 2.00, 0.0, 0.90, 2.5, 0.80, 7.5, 8.5, 2
point.2=1, 1.74, 10.00, -9.30, 2200, 2, 2.00, 0.0, 0.90, 2.5, 0.80, 8.0, 7.0, 3
point.3=2, 0.00, -41.00, 2.30, 1200, 0, 0.00, 0.0, 0.00, 0.0, 0.00, 0.0, 0.0, 5
point.4=2, 0.00, 41.00, 2.30, 1200, 0, 0.00, 0.0, 0.00, 0.0, 0.00, 0.0, 0.0, 6
point.5=2, -42.00, 0.00, -1.00, 1200, 0, 0.00, 0.0, 0.00, 0.0, 0.00, 0.0, 0.0, 9
point.6=2, 17.16, 0.00, -2.83, 1200, 0, 0.00, 0.0, 0.00, 0.0, 0.00, 0.0, 0.0, 4
static_pitch = 7.44 //degrees (pitch when loaded on ground)
static_cg_height= 8.167 //(feet) altitude of CG when at rest (altitude when loaded on ground)
[Views]
eyepoint=-4.56, 0.00, 3.21 //(feet) longitudinal, lateral, vertical distance from reference datum
[fuel]
LeftMain= -3.000, -12.000, 1.600, 857.500, 0.000
RightMain= -3.000, 12.000, 1.600, 857.500, 0.000
fuel_type= 1.000
number_of_tank_selectors= 1
[airplane_geometry]
wing_area= 841.000
wing_span= 81.667
wing_root_chord= 10.417
wing_dihedral= 6.801
wing_incidence= 1.000
wing_twist= 0.000
oswald_efficiency_factor= 0.725
wing_winglets_flag= 0
wing_sweep= 0.000
wing_pos_apex_lon= 0.000
wing_pos_apex_vert= 0.000
htail_area= 331.000
htail_span= 43.000
htail_pos_lon= -38.750
htail_pos_vert= 0.000
htail_incidence= 0.000
htail_sweep= 0.000
vtail_area= 220.000
vtail_span= 16.912
vtail_sweep= 0.000
vtail_pos_lon= -38.750
vtail_pos_vert= 7.167
elevator_area= 94.410
aileron_area= 80.250
rudder_area= 39.490
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
[Flaps.0]
type= 1
span-outboard= 0.500
extending-time= 5.000
system_type= 0
flaps-position.0= 0.000, 0.000
flaps-position.1= 15.000, 0.000
flaps-position.2= 30.000, 0.000
flaps-position.3= 45.000, 0.000
[GeneralEngineData]
engine_type= 0
Engine.0= 11.417, -10.000, 0.000
Engine.1= 11.417, 10.000, 0.000
fuel_flow_scalar= 1.000
[Reference Speeds]
flaps_up_stall_speed= 83.000
full_flaps_stall_speed= 66.400
cruise_speed= 237.054
[keyboard_response]
elevator= 350.000, 500.000
aileron= 450.000, 1000.000
rudder= 200.000, 1000.000
[General]
performance=
[autopilot]
autopilot_available= 1
flight_director_available= 0
default_vertical_speed= 700.000
autothrottle_available= 0
pitch_takeoff_ga= 8.000
autoland_available= 1
