[fltsim.0]
title=Goevier III
sim=Goevier
model=
panel=
sound=
texture=
kb_reference=goevier_ref
kb_checklists=goevier_check
description="Goevier III, a two seat glider (side-by-side) for training 1937-1943( Gö-4 II ) and later 1951-1954( Gö-4 III )"
ui_manufacturer=Schempp Hirth
ui_type=Goevier III
ui_typerole="Glider"
ui_createdby"Wolfgang Piper"
ui_variation=


[General]
performance=Span: 14.8 m\nEmpty Weight: 235 kg, Gross weight 410 kg\nMin. sink: 0.90 m/s at 60 km/h\nL/D max: 20 at 70 km/h\nV min: 55 km/h\nV max: 170 km/h
Category=airplane




[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 = .75
ShowWeather = Yes
InitialXyz = 0, 3.1, -20.0
InitialPbh = 10, 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 = 12.5, 1.9, 0.0
InitialPbh = 9, 0, 270
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 = -12.5, 1.9, 0.0
InitialPbh = 9, 0, 90
XyzAdjust = TRUE
Category=Aircraft
MomentumEffect = TRUE
ClipMode=Minimum

[CameraDefinition.001]
Title = "Right Seat"
Guid = {195EAB58-9E4A-4E2A-A34C-A8D9D948F078}
Origin = Virtual Cockpit
MomentumEffect = Yes
SnapPbhAdjust = Swivel
SnapPbhReturn = False
PanPbhAdjust = Swivel
PanPbhReturn = False
Track = None
ShowAxis = YES
AllowZoom = TRUE
InitialZoom = .7
SmoothZoomTime = 2.0
ZoomPanScalar = 1.0
ShowWeather = Yes
XyzAdjust = TRUE
ShowLensFlare=FALSE
Category = Cockpit
PitchPanRate=30
HeadingPanRate=75
PanAcceleratorTime=0
InitialXyz=0.32, 0.00, 0.00
InitialPbh=0, 0, 0






[electrical]
max_battery_voltage=24
avionics_bus=0, 0 , 0
avionics=0, 0 , 0
additional_system=0, 0 , 0
flap_motor=0, 0 , 0
gear_motor=0, 0 , 0


[WEIGHT_AND_BALANCE]

reference_datum_position=0,0,0
empty_weight_CG_position=-3.5,0,0,0
max_number_of_stations=5
station_load.0="180, 0.5,0,0,Pilot"       
station_load.1="180, 0.5,0,0,Guest"       
empty_weight=470.000000
empty_weight_roll_MOI=1000.000000
empty_weight_pitch_MOI=2000.000000
empty_weight_yaw_MOI=1000.000000
empty_weight_coupled_MOI=0.000000
max_gross_weight=904.000000
CG_forward_limit= 0.150  
CG_aft_limit=     0.350  




[flight_tuning]
cruise_lift_scalar=1.4
parasite_drag_scalar=1.1
induced_drag_scalar=1.2
elevator_effectiveness=1.5
aileron_effectiveness=1.5
rudder_effectiveness=1.0
pitch_stability=1.1
roll_stability=1.0
yaw_stability=1.0
elevator_trim_effectiveness=1.2
aileron_trim_effectiveness=1.0
rudder_trim_effectiveness=1.0

[airplane_geometry]
wing_area=165.000000
wing_span=48
wing_root_chord=5
wing_dihedral=1
wing_incidence=5
wing_twist=1
oswald_efficiency_factor=0.7
wing_winglets_flag=0
wing_sweep=0.000000
wing_pos_apex_lon=0
wing_pos_apex_vert=1.000000
htail_area=22.000000
htail_span=9
htail_pos_lon=-12
htail_pos_vert=2.000000
htail_incidence=2.000000
htail_sweep=0.000000
vtail_area=15
vtail_span=5
vtail_sweep=0.000000
vtail_pos_lon=-10
vtail_pos_vert=2
elevator_area=4
aileron_area=11.900000
rudder_area=3
elevator_up_limit=27
elevator_down_limit=15
aileron_up_limit=17
aileron_down_limit=10
rudder_limit=23.491270
elevator_trim_limit=35
spoiler_limit=59.988681
spoilerons_available=0
aileron_to_spoileron_gain=0.000000
min_ailerons_for_spoilerons=0.000000
min_flaps_for_spoilerons=0.000000
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=-3.500000
negative_g_limit_flaps_down=-3.500000



 
[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

 

//          Lang.   Breit.  Vert.
//          Pos.    Pos.    Pos.
//  0        1       2       3       4     5    6        7       8       9       10      11    12    13    14    15
//-------------------------------------------------------------------------------------------------------------------------------- 



point.0=1, -13.5,   0,    -0.61,  1574.8,  0,   0.5062,  0,      0.2,    2,     0.35,   0.6,  0.6,  0,    0,    0    // Gear Tail
point.1=1, 0.9,    0.1,   -1.75,  1574.8,  1,   0.509,   0,      0.2,    2,     0.50,   0.6,  0.6,  2,    0,    0    // Gear Main
point.2=1, 0.9,    0.2,   -1.75,  1574.8,  2,   0.509,   0,      0.2,    2,     0.50,   0.6,  0.6,  2,    0,    0    // Gear Main
point.3=2, 0.15,    -24,  1.50,   1574.4,  0,   0,       0,      0,      0,      0,      0,    0,    5,    0,    0    // Wing Tip
point.4=2, 0.15,     24,  1.50,   1574.4,  0,   0,       0,      0,      0,      0,      0,    0,    6,    0,    0    // Wing Tip
point.5=2, -13.8,  0,     -0.28,  1574.4,  0,   0,       0,      0,      0,      0,      0,    0,    9,    0,    0    // Tail
point.6=2, 3.6,    0,     -1.53,  1574.4,  0,   0,       0,      0,      0,      0,      0,    0,    4,    0,    0    // Nose

 
//Converted with CPA V.1.05 by Wolfgang Piper
//20. July 2004


static_pitch=6
static_cg_height=1.8

gear_system_type=0

[Views]
eyepoint=1.36,-0.61, 1.72

 

 
[GeneralEngineData]
engine_type=2
fuel_flow_scalar=1.000000

[Reference Speeds]
flaps_up_stall_speed=35.000000
full_flaps_stall_speed=34.00000
cruise_speed=45.0000
max_indicated_speed=250


[keyboard_response]
elevator=60.000000,90.000000
aileron=60.000000,90.000000
rudder=60.000000,90.000000

[autopilot]
autopilot_available=0
flight_director_available=0

[direction_indicators]
direction_indicator.0=0,0

[fuel]
fuel_type=1.000000

[brakes]
toe_brakes_scale=1.000031
parking_brake=1

[gear_warning_system]
gear_warning_available=0
pct_throttle_limit=0.000000
flap_limit_power=0.000000
flap_limit_idle=0.000000

[hydraulic_system]
normal_pressure=0.000000

[stall_warning]
type=1
stick_shaker=0

[attitude_indicators]
attitude_indicator.0=1

[variometers]
variometer.0=54,-116	

[turn_indicators]
turn_indicator.0=1,0
[Flaps.0]
type=0
span-outboard=0.500000
extending-time=0.000000
system_type=0
[pitot_static]
pitot_heat=0.000000
[vacuum_system]
max_pressure=0.000000
vacuum_type=0
electric_backup_pressure=0.000000
engine_map=1,1,1,1
[pneumatic_system]
max_pressure=0.000000
bleed_air_scalar=0.000000
[deice_system]
structural_deice_type=0