[fltsim.0]
title=genesis2
sim=genesis2
model=
panel=
sound=
texture=
kb_checklists=
kb_checklists=
kb_reference=
description=The GENESIS 2 is a modern Standard Class racing sailplane of unusual configuration . It is made of composite materials, with a self-stable wing, utilising the latest design and aeronautical construction technology. Designer : David Rowberry
ui_manufacturer=L.A.K.
ui_type=Genesis 2
ui_typerole="Glider"
ui_createdby=David Rowberry
ui_variation=
atc_heavy=0
atc_id=
atc_airline=
atc_flight_number=

[CameraDefinition.0]
Title=Tail
Guid = {5c1df273-034b-4e7f-953a-9d5e26f1646c}
Description = Looking forward from behind the aircraft
Origin = Center
SnapPbhAdjust = Swivel
SnapPbhReturn = FALSE
PanPbhAdjust = Swivel
PanPbhReturn = FALSE
Track = None
ShowAxis = FALSE
AllowZoom = TRUE
InitialZoom = .5
ShowWeather = Yes
InitialXyz = 0.0, 1.5, -5.0
InitialPbh = 15, 0, 0
XyzAdjust = TRUE
Category=Aircraft
MomentumEffect=TRUE
ClipMode=Minimum



[CameraDefinition.1]
Title=Right Wing
Guid = {C690EAFD-223A-42d0-99E0-681ADF93BB59}
Description = View from the right wing tip looking at the cockpit
Origin = Center
SnapPbhAdjust = Swivel
SnapPbhReturn = FALSE
PanPbhAdjust = Swivel
PanPbhReturn = FALSE
Track = None
ShowAxis = FALSE
AllowZoom = TRUE
InitialZoom = 0.5
ShowWeather = Yes
InitialXyz = 8.0, 0.5, 1.0
InitialPbh = 0, 0, 265
XyzAdjust = TRUE
Category=Aircraft
MomentumEffect = TRUE
ClipMode=Minimum


[CameraDefinition.2]
Title=Left Wing
Guid = {33320004-b71a-4f9f-9105-1eb674ab7f3c}
Description = View from the left wing tip looking at the cockpit
Origin = Center
SnapPbhAdjust = Swivel
SnapPbhReturn = FALSE
PanPbhAdjust = Swivel
PanPbhReturn = FALSE
Track = None
ShowAxis = FALSE
AllowZoom = TRUE
InitialZoom = 0.5
ShowWeather = Yes
InitialXyz = -11.5, 0.5, 0.5
InitialPbh = 0, 0, 95
XyzAdjust = TRUE
Category=Aircraft
MomentumEffect = TRUE
ClipMode=Minimum

[CameraDefinition.3]
Title=Nose
Guid = {59181B43-9231-4fb0-8FF7-FB4318532141}
Description =Looking back from the nose of the glider
Origin = Center
SnapPbhAdjust = Swivel
SnapPbhReturn = FALSE
PanPbhAdjust = Swivel
PanPbhReturn = FALSE
Track = None
ShowAxis = FALSE
AllowZoom = TRUE
InitialZoom = .5
ShowWeather = Yes
InitialXyz = 1, 0.1, 3.0
InitialPbh = 2, 0, 190
XyzAdjust = TRUE
Category=Aircraft
MomentumEffect=FALSE
ClipMode=Minimum



[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 -15 m\nWt empty - 240 kg , all up - 525 kg\nMin Sink - 85 kph\nbest glide - 124 kph\nVNE - 276 kph\nStall - 75 kph\n
Category=airplane
atc_type=
atc_model=

[WEIGHT_AND_BALANCE]
max_gross_weight = 1157.000
empty_weight = 530.000

reference_datum_position     = 0.000, 0.000, 0.000
empty_weight_CG_position     = 0.75, 0.000, 0.000

max_number_of_stations = 5

station_load.0 =170.000000, 0.000000, 0.000000, 0.000000, Pilot          
//station_load.1 =130.000000, 0.000000, 0.000000, 0.000000, ballast

empty_weight_pitch_MOI   = 1063.000
empty_weight_roll_MOI    = 602.000
empty_weight_yaw_MOI     = 659.000
empty_weight_coupled_MOI = 0.000
CG_forward_limit= 0.000
CG_aft_limit= 1.000


[flight_tuning]
cruise_lift_scalar     =1.12
parasite_drag_scalar   =0.89
induced_drag_scalar    =1.05
elevator_effectiveness =1.00
aileron_effectiveness  =0.40
rudder_effectiveness   =0.60
pitch_stability        =1.00
roll_stability         =1.00
yaw_stability          =1.00
elevator_trim_effectiveness =1.901
aileron_trim_effectiveness  =1.000
rudder_trim_effectiveness   =1.000

[GeneralEngineData]
engine_type= 2
fuel_flow_scalar= 5.000

[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, 3.875, 0.000, -2.46, 1000.000, 0.000, 0.600, 0.000, 0.100, 2.000, 0.750, 2.000, 1.500, 0.000, 0.000, 0.000
point.1= 1.000, -1.220, 0.001, -2.85, 1000.000, 1.000, 0.800, 0.000, 0.300, 2.500, 0.750, 2.000, 1.500, 2.000, 0.000, 0.000
point.2= 1.000, -1.220,-0.001, -2.85, 1000.000, 0.000, 0.800, 0.000, 0.300, 2.500, 0.750, 2.000, 1.500, 2.000, 0.000, 0.000
point.3= 2.000, 0.920, 23.318, 0.55, 700.000,  0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 6.000, 0.000, 0.000
point.4= 2.000, 0.920,-23.318, 0.62, 700.000,  0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 5.000, 0.000, 0.000
point.5= 2.000,-4.570, 0.000, -0.95, 1000.000, 0.000, 0.000, 0.000, 0.100, 2.000, 0.750, 0.000, 0.000, 4.000, 0.000, 0.000
point.6= 2.000, 2.370, 0.000, -2.04, 1275.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 9.000, 0.000, 0.000


static_pitch= -0.80
static_cg_height= 2.40
gear_system_type=3

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

[fuel]
electric_pump=0
fuel_type = 2                                //Fuel type: 1 = Avgas, 2 = JetA
Center1= 0.000, 0.000, 0.000, 0.000, 0.000
number_of_tank_selectors=1



[Views]
eyepoint = 1.0, 0.0, 0.3

[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, 1
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_s

[airplane_geometry]
wing_area               = 120
wing_span               = 49.26
wing_root_chord         = 3.878
wing_dihedral           = 4.000
wing_incidence          = 3.000
wing_twist              = -2.000
oswald_efficiency_factor= 0.800
wing_winglets_flag      = 0
wing_sweep              = -2.000
wing_pos_apex_lon       = 0.75
wing_pos_apex_vert      = 0.000
htail_area              = 6.300
htail_span              = 5.800
htail_pos_lon           = -8.178
htail_pos_vert          = 4.665
htail_incidence         = 0.000
htail_sweep             = 0.000
vtail_area              = 5.300
vtail_span              = 4.500
vtail_sweep             = 20.000
vtail_pos_lon           = -5.400
vtail_pos_vert          = 4.665
elevator_area           = 6.300
aileron_area            = 7.280
rudder_area             = 3.000
elevator_up_limit       = 24.000
elevator_down_limit     = 24.000
aileron_up_limit        = 20.000
aileron_down_limit      = 15.000
rudder_limit            = 25.000
elevator_trim_limit     = 20.000
spoiler_limit           = 60.000
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=5.500000
positive_g_limit_flaps_down=5.500000
negative_g_limit_flaps_up=-3.550000
negative_g_limit_flaps_down=-3.580000

[Reference Speeds]
flaps_up_stall_speed    = 43.000
full_flaps_stall_speed  = 43.000
cruise_speed            = 67.000
max_indicated_speed     = 150                   //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= 0.000
extending-time= 0.100
system_type= 3
damaging-speed= 0.000
blowout-speed= 0.000
lift_scalar= 0.000
drag_scalar= 0.000
pitch_scalar= 0.000

[Water Ballast System]
//Tank.n =  Gallons,  Long,    Lat,   Vert,  iValve
Tank.0  = 25.00, -0.66,  -4.5, 0.0, 1          //Left Inboard
Tank.1  = 25.00, -0.66,   4.5, 0.0, 1          //Right Inboard

NumberOfReleaseValves = 1
DumpRate = 0.18494                            //Gallons per second


[hydraulic_system]
normal_pressure=0.000000