[fltsim.0]
title=Segway
sim=Segway
model=
panel=
sound=
texture=
kb_checklists=Curtiss_Jenny_check
kb_reference=Curtiss_Jenny_ref
atc_id=
atc_id_color=
ui_manufacturer=Flyways
ui_type=Segway
ui_variation=i180
description="The Segway Human Transporter (HT) i180 is our most versatile and colorful model. With new fenders, wheels and battery options, it was designed for extended range, stability and plenty of cargo capacity. The i180 readily navigates a wide range of operating environments and terrain."
[General]
atc_type=Experimental
atc_model=Jenny
editable=1
performance="Maximum Speed\n12.5 mph"
[WEIGHT_AND_BALANCE]
max_gross_weight = 600 // (pounds)
empty_weight = 400 // (pounds)
reference_datum_position = 0, 0, 0 // (feet) distance from FlightSim Reference position: (1/4 chord, centerline, waterline)
empty_weight_CG_position = 0, 0, -4.5 // (feet) longitudinal, lateral, vertical distance from specified datum
max_number_of_stations =1
station_load.0 = "165.000, 0.0, 0.0, 0.0, Pilot" // Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
;Moments of Inertia
empty_weight_pitch_MOI = 1005.8
empty_weight_roll_MOI = 1034.6
empty_weight_yaw_MOI = 2093.7
empty_weight_coupled_MOI = 0.0
[flight_tuning]
cruise_lift_scalar = 0.3
parasite_drag_scalar = 0.5
induced_drag_scalar = 0.5
elevator_effectiveness = 0.1
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= 0
[GeneralEngineData]
engine_type = 0 //0=Piston, 1=Jet, 2=None, 3=Helo-Turbine, 4=Rocket, 5=Turboprop
Engine.0 = 0.0, 0.0, -4.0 //(feet) longitudinal, lateral, vertical distance from reference datum
fuel_flow_scalar= 0.5 //Fuel flow scalar
min_throttle_limit = 0.0 //Minimum percent throttle. Generally negative for turbine reverser
starter_type = 1 //1=Manual Starter
[piston_engine]
power_scalar = 1.0 //Piston power scalar
cylinder_displacement= 60.0 //Cubic inches per cylinder
compression_ratio= 5.4 //Compression ratio
number_of_cylinders=4 //Number of cylinders
number_of_magnetos = 1 //Number of magnetos
max_rated_rpm= 400 //Max rated RPM
max_rated_hp= 90 //Max rated HP
fuel_metering_type= 0 //0=Fuel Injected, 1=Gravity Carburetor, 2=Aerobatic Carburetor
cooling_type= 1 //0=Cooling type Air, 1=Cooling type Liquid
normalized_starter_torque= 0.3 //Starter torque factor
turbocharged= 0 //Is it turbocharged? 0=FALSE, 1=TRUE
max_design_mp= 0 //Max design manifold pressure, (inHg)
min_design_mp= 0 //Min design manifold pressure, (inHg)
critical_altitude= 0 //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= 0.9 //Scalar on maximum RPM mechanical efficiency
idle_rpm_mechanical_efficiency_scalar= 0.9 //Scalar on idle RPM mechanical efficiency
max_rpm_friction_scalar= 0.9 //Scalar on maximum RPM friction
idle_rpm_friction_scalar= 0.9 //Scalar on idle RPM friction
[propeller]
propeller_type=1
propeller_diameter=6.883000
propeller_blades=2
propeller_moi=5.706520
beta_max=12.521739
beta_min=15.000000
min_gov_rpm=0.000000
prop_tc=0.100000
gear_reduction_ratio=1.000000
fixed_pitch_beta=20.000000
low_speed_theory_limit=80.000000
prop_sync_available=0
prop_deice_available=0
prop_feathering_available=0
prop_auto_feathering_available=0
min_rpm_for_feather=0.000000
beta_feather=0.000000
power_absorbed_cf=0.000000
defeathering_accumulators_available=0
prop_reverse_available=0.000000
minimum_on_ground_beta=0.000000
minimum_reverse_beta=0.000000
//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
[contact_points]
point.0=1, 2.0, 0.0, -6.2, 8000.0, 0, 0.50, 80.0, 0.4, 2.5, 1.2, 0.0, 0.0, 0
point.1=1, -2.0, -3.0, -6.2, 8000.0, 1, 0.50, 0.0, 0.4, 2.5, 1.2, 0.0, 0.0, 2
point.2=1, -2.0, 3.0, -6.2, 8000.0, 2, 0.50, 0.0, 0.4, 2.5, 1.2, 0.0, 0.0, 3
static_pitch = 9.44
static_cg_height = 4.64
[brakes]
parking_brake = 1 //Parking brake available
toe_brakes_scale = 1.0 //Brake scalar
auto_brakes=0
[hydraulic_system]
normal_pressure = 0.0 //PSI
[Views]
eyepoint = 0.0, 0.0, 0.80
[LIGHTS]
//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing
light.0 = 4, -4.0, 0.00, 1.80, fx_vclight,
[Radios]
// Radio Type = availiable, standby frequency, has glide slope
Audio.1 = 0
Com.1 = 1, 0
Nav.1 = 0, 0, 0
Adf.1 = 0
Transponder.1 = 0
Marker.1 = 0
[keyboard_response]
//Breakpoint speeds (knots) on the keyboard increments of control surfaces.
//Speed at which the incremenet is reduced to 1/2 and 1/8 respectively.
elevator =200, 1000
aileron =200, 1000
rudder =200, 1000
[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=0,0
[attitude_indicators]
//Type: 0=None, 1=Vacuum Gyro, 2=Electric Gyro
attitude_indicator.0 = 0
[turn_indicators]
//Type: 0=None, 1=Electric Gyro, 2=Vacuum Gyro
turn_indicator.0=0,0
[EFFECTS]
wake=fx_wake
water=fx_spray
dirt=fx_tchdrt
concrete=fx_sparks
touchdown=fx_tchdwn_s, 1
windshield_rain_effect_available = 0 //Do not draw rain on this windshield
[electrical]
max_battery_voltage = 0
generator_alternator_voltage = 0
[fuel]
Center1 = 0.0, 0.0, -1.0, 21.0, 0.0 //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)
fuel_type = 1 //Fuel type: 1 = Avgas, 2 = JetA
number_of_tank_selectors = 1
electric_pump=0
[airplane_geometry]
wing_area = 1.0 //Square feet
wing_span = 10.0 //Feet
wing_root_chord = 1.0 //Feet
wing_dihedral = 1.0 //Degrees
wing_incidence = 2.0 //Degrees
wing_twist = 0.0 //Degrees
oswald_efficiency_factor= 1.0 //Measure of lift effeciency of wing (Artificially high for biplanes)
wing_winglets_flag = 0 //Are winglets available?
wing_sweep = 0.0 //Degrees, wing leading edge
wing_pos_apex_lon = 0.85 //Feet, longitudinal distance from reference point, negative going aft
wing_pos_apex_vert = 1.4 //Feet, vertical distance from reference point, positive going up
htail_area = 10.0 //Square feet
htail_span = 10.0 //Feet
htail_pos_lon = -16.6 //Feet, longitudinal distance from reference point, negative going aft
htail_pos_vert = -1.1 //Feet, vertical distance from reference point, positive going up
htail_incidence = 0.0 //Degrees
htail_sweep = 0.0 //Degrees, horizontal tail leading edge
vtail_area = 15.0 //Square feet
vtail_span = 6.0 //Feet, tip to body
vtail_sweep = 39.0 //Degrees, vertical tail leading edge
vtail_pos_lon = -18.9 //Feet, longitudinal distance from reference point, negative going aft
vtail_pos_vert = 1.4 //Feet, vertical distance from reference point, positive going up
elevator_area = 1.0 //Square feet
aileron_area = 10.0 //Square feet
rudder_area = 10.0 //Square feet
elevator_up_limit = 30.0 //Degrees
elevator_down_limit = 20.0 //Degrees
aileron_up_limit = 20.0 //Degrees
aileron_down_limit = 20.0 //Degrees
rudder_limit = 25.0 //Degrees
elevator_trim_limit = 0.0 //Degrees
spoiler_limit = 0.0 //Degrees
spoilerons_available = 0 //Spoilerons Available?
aileron_to_spoileron_gain = 0 //Aileron to spoileron gain
min_ailerons_for_spoilerons = 0 //Degrees
min_flaps_for_spoilerons = 0 //Minimum flap handle position when spoilerons activate
auto_spoiler_available=0
[Reference Speeds]
flaps_up_stall_speed = 39.0 //Knots True (KTAS)
full_flaps_stall_speed = 39.0 //Knots True (KTAS)
cruise_speed = 54.7 //Knots True (KTAS)
max_indicated_speed = 180 //Red line (KIAS)
[autopilot]
autopilot_available= 0
flight_director_available= 0
[forcefeedback]
ground_bumps_magnitude1=2600 ; 0 - 10000
ground_bumps_angle1=8900 ; 0 - 35999 degrees
ground_bumps_intercept1=5.0
ground_bumps_slope1=0.6
ground_bumps_magnitude2=1200 ; 0 - 10000
ground_bumps_angle2=9100 ; 0 - 35999 degrees
ground_bumps_intercept2=0.085
ground_bumps_slope2=0.65
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=3500000 ; in microseconds
[stall_warning]
type=0
stick_shaker=0
[exits]
number_of_exits = 0
[pitot_static]
pitot_heat=1.000000
