[fltsim.0]
title=swift
sim=swift
model=
panel=
sound=
texture=
kb_checklists=
kb_checklists=
kb_reference=
description=The SWIFT is a high performance foot-launched sailplane, designed to combine some of the convenience of hang gliders with the soaring performance of sailplanes. It takes off and lands like a hang glider, yet maintains exceptional performance at high speeds, achieving a lift-to-drag ratio of about 25:1. Although it is a fully-cantilevered rigid wing with aerodynamic controls and flaps, it weighs only about 100 lbs and is easily transported on the top of a car
ui_manufacturer=Aeriane
ui_type=Swift'Light
ui_typerole="Glider"
ui_createdby=David Rowberry
ui_variation=
atc_heavy=0
atc_id=
atc_airline=
atc_flight_number=



[Electrical]
max_battery_voltage=12.0
additional_system=0,0.0,0
avionics_bus=0,0.1,1
avionics=5,0.1,1



[General]
performance=Span - 12.8 m\nWt empty - 48 kg , all up - 158 kg\nMin Sink 0.6m\/s @43km\/h\nbest glide - 27:1 @70km\/h kph\nVNE - 120 km\/h\nStall - 32 km\/h\n
Category=airplane
atc_type=
atc_model=

[WEIGHT_AND_BALANCE]
max_gross_weight = 347.000
empty_weight = 126.000

reference_datum_position     = 2.386, 0.000, 1.276
empty_weight_CG_position     = -2.300, 0.000, 0.000

max_number_of_stations = 2

station_load.0 =170.000000, -0.500000, 0.000000, 0.000000, Pilot          
station_load.1 =40.000000, 0.000000, 0.000000, 0.000000, ballast

empty_weight_pitch_MOI   = 302.000
empty_weight_roll_MOI    = 924.000
empty_weight_yaw_MOI     = 859.000
empty_weight_coupled_MOI = 0.000
CG_forward_limit= 0.000
CG_aft_limit= 1.000


[flight_tuning]
cruise_lift_scalar     =1.0
parasite_drag_scalar   =1.0
induced_drag_scalar    =1.0
elevator_effectiveness =1.4
aileron_effectiveness  =1.5
rudder_effectiveness   =1.0
pitch_stability        =0.7
roll_stability         =0.7
yaw_stability          =0.6
elevator_trim_effectiveness =1.904
aileron_trim_effectiveness  =1.000
rudder_trim_effectiveness   =1.000

[GeneralEngineData]
engine_type= 1
engine.0= 0.000, 0.000, 0.000
fuel_flow_scalar= 1.000
static_thrust=250
min_throttle_limit=0.000000

[pitot_static]
vertical_speed_time_constant = 4                //Increasing this value will cause a more instantaneous reaction in the VSI
pitot_heat=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= 1.000, 0.248, 0.000, -3.650, 700.000, 1.000, 0.250, 0.000, 0.300, 2.500, 0.750, 0.000, 0.000, 0.000, 0.000, 0.000
point.1= 1.000, -4.827, 0.000, -3.300, 700.000, 0.000, 0.250, 0.000, 0.300, 2.500, 0.750, 0.000, 0.000, 0.000, 0.000, 0.000
point.2= 2.000, -5.886, 18.800, -0.400, 500.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 6.000, 0.000, 0.000
point.3= 2.000, -5.386, -18.800, -0.400, 500.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 5.000, 0.000, 0.000


static_pitch= 0.000
static_cg_height= 1.972
gear_system_type=3

[brakes]
parking_brake = 1        //Parking brake available
toe_brakes_scale = 0.27  //Brake scalar

[fuel]
electric_pump=1
fuel_type = 2                                //Fuel type: 1 = Avgas, 2 = JetA
Center1= 0.000, 0.000, 0.000, 0.250, 0.000
number_of_tank_selectors=1

[TurbineEngineData]
fuel_flow_gain= 0.022
inlet_area= 1.808
rated_N2_rpm= 29920.000
static_thrust= 250.000
afterburner_available= 0
reverser_available= 0.000

[jet_engine]
thrust_scalar=1.000


[hydraulic_system]
normal_pressure = 0.0    //PSI

[Views]
eyepoint = -2.3, 0.0, -1.2

[LIGHTS]
//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing
light.0 = 4,  2.7,   0.00,  1.50, fx_vclight,

[variometers]
variometer.0=54,-116	


[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 = 160, 360
aileron  = 160, 360
rudder   = 160, 360

[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_tchdwn

[airplane_geometry]
wing_area               = 136.000
wing_span               = 42.000
wing_root_chord         = 4.000
wing_dihedral           = 0.000
wing_incidence          = -3.000
wing_twist              = 2.000
oswald_efficiency_factor= 0.600
wing_winglets_flag      = 1
wing_sweep              = 20.000
wing_pos_apex_lon       = 1.000
wing_pos_apex_vert      = 0.000
htail_area              = 0.100
htail_span              = 0.100
htail_pos_lon           = 0.000
htail_pos_vert          = 0.000
htail_incidence         = 0.000
htail_sweep             = 0.000
vtail_area              = 20.000
vtail_span              = 4.300
vtail_sweep             = 20.000
vtail_pos_lon           = -7.300
vtail_pos_vert          = 0.000
elevator_area           = 9.430
aileron_area            = 9.430
rudder_area             = 6.600
elevator_up_limit       = 15.000
elevator_down_limit     = 9.000
aileron_up_limit        = 16.000
aileron_down_limit      = 10.000
rudder_limit            = 40.000
elevator_trim_limit     = 15.000
spoiler_limit           = 70.000
spoilerons_available    = 0
aileron_to_spoileron_gain = 0.000
min_ailerons_for_spoilerons = 0.000
min_flaps_for_spoilerons = 0.000
auto_spoiler_available=0
spoiler_extension_time=0.500000
positive_g_limit_flaps_up=5.300000
positive_g_limit_flaps_down=5.300000
negative_g_limit_flaps_up=-2.6500000
negative_g_limit_flaps_down=-2.6500000

[Reference Speeds]
flaps_up_stall_speed    = 12.400
full_flaps_stall_speed  = 10.700
cruise_speed            = 37.800
max_indicated_speed     = 64.8                   //Red line (KIAS)
max_mach=0.260010

[autopilot]
autopilot_available= 0
flight_director_available= 0

[forcefeedback]
ground_bumps_magnitude1=2500            ; 0 - 10000
ground_bumps_angle1=8900                ; 0 - 35999 degrees
ground_bumps_intercept1=10.0
ground_bumps_slope1=0.300
ground_bumps_magnitude2=350             ; 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

[yaw_string]
yaw_string_available=1

[stall_warning]
type=1
stick_shaker=0


[vacuum_system]
max_pressure=5.150000
vacuum_type=0
electric_backup_pressure=0.000000
engine_map=0,0,0,0

[pneumatic_system]
max_pressure=0.000000
bleed_air_scalar=0.000000

[deice_system]
structural_deice_type=0
[gear_warning_system]
gear_warning_available=1
pct_throttle_limit=0.000000
flap_limit_power=0.000000
flap_limit_idle=0.000000

[Flaps.0]
type= 1
span-outboard= 0.500
extending-time= 2.500
system_type= 3
damaging-speed= 43.000
blowout-speed= 50.000
lift_scalar= -1.00
drag_scalar= 0.000
pitch_scalar= 0.000
flaps-position.0= 0.000, 0.000
flaps-position.1= 5.000, 0.000
flaps-position.2= 15.000, 0.000
flaps-position.3= 25.000, 0.000
flaps-position.4= 35.000, 0.000
flaps-position.5= 45.000, 0.000