[fltsim.0]
title=SupaPup
sim=Supapup
model=
panel=
panel_alias = c172\panel
sound=
sound_alias = c172\sound
texture=
kb_checklists=
kb_reference=
prop_anim_ratio=-1.5
atc_id=PUP
ui_manufacturer=SupaPup
ui_type=SupaPupMkIV
ui_variation=Silver and Black
description=SupaPup MkIV Sports aircraft modeled by Gilles Arlove\nThe Supapup is a single seat homebuilt aircraft that can be registered as an ultralight or experimantal catergory. This example is modeled after a Supapup based at Latrobe Valley airport Victoria , Australia.\[email protected]
atc_heavy=0
atc_airline=
atc_flight_number=
visual_damage=0

[fltsim.1]
title=SupaPup Blue
sim=Supapup
model=1
panel=
panel_alias = c172\panel
sound=
sound_alias = c172\sound
texture=1
kb_checklists=
kb_reference=
prop_anim_ratio=-1.58
atc_id=PUP
ui_manufacturer=SupaPup
ui_type=SupaPupMkIV
ui_variation=White and Blue
description=SupaPup MkIV Sports aircraft modeled by Gilles Arlove\nThe Supapup is a single seat homebuilt aircraft that can be registered as an ultralight or experimantal catergory. This example is modeled after a Supapup based at Latrobe Valley airport Victoria , Australia.\[email protected]
atc_heavy=0
atc_airline=
atc_flight_number=
visual_damage=0



[General]
atc_type=Supapup	
atc_model=Supapup
performance=Cruise speed: 95kts\nStall Speed :   36kts\nEmpty Weight : 210 KG\nMTOW:            360KG\nPowerplant: Jabiru 54HP 4 stroke engine

[WEIGHT_AND_BALANCE]
max_gross_weight = 900.000
empty_weight = 600.000

reference_datum_position     = 3.600, 0.000, 0.000
empty_weight_CG_position     = -3.000, 0.000, -1.000

max_number_of_stations = 50

station_load.0 = 170.000, -3.000, -1.500, 0.000
station_load.1 = 170.000, -3.000, 1.500, 0.000
station_load.2 =   0, -6.2, -1.5, 0.0           //Rear Passenger  Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.3 =   0, -6.2,  1.5, 0.0           //Rear Passenger  Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.4 =   0, -8.0,  0.0, 0.0           //Baggage         Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)

;Moments of Inertia
empty_weight_pitch_MOI  = 1400.000
empty_weight_roll_MOI   = 1137.000
empty_weight_yaw_MOI    = 2360.000
empty_weight_coupled_MOI= 0.000
CG_forward_limit= 0.000
CG_aft_limit= 1.000


[flight_tuning]
cruise_lift_scalar     =1.000
parasite_drag_scalar   =1.804
induced_drag_scalar    =2.002
elevator_effectiveness =1.000
aileron_effectiveness  =1.000
rudder_effectiveness   =1.000
pitch_stability        =1.000
roll_stability         =1.000
yaw_stability          =1.000
elevator_trim_effectiveness =1.000
aileron_trim_effectiveness  =1.000
rudder_trim_effectiveness   =1.000

[GeneralEngineData]
engine_type = 0
Engine.0 = 2.400, 0.000, 0.000
fuel_flow_scalar= 0.880

[piston_engine]
power_scalar =1.000
cylinder_displacement= 70.000
compression_ratio= 8.500
number_of_cylinders= 4
max_rated_rpm= 2700.000
max_rated_hp= 60.000
fuel_metering_type= 1
cooling_type= 0
normalized_starter_torque= 0.300
turbocharged= 0
max_design_mp= 0.000
min_design_mp= 0.000
critical_altitude= 0.000
emergency_boost_type= 0
emergency_boost_mp_offset= 0.000
emergency_boost_gain_offset= 0.000
fuel_air_auto_mixture= 0
auto_ignition= 0
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 =1.000
propeller_type= 1
rotation=-1
propeller_diameter= 6.000
propeller_blades= 2
propeller_moi= 5.000
beta_max= 0.000
beta_min= 0.000
min_gov_rpm= 0.000
prop_tc= 0.000
gear_reduction_ratio= 1.000
fixed_pitch_beta= 18.500
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

[electrical]
                ;BusType, MaxAmpLoad, MinVoltage       BusTypes:0=MainBus,1=AvionicsBus,2=BatteryBus,3=HotBatteryBus,4-7=Generator/AlternatorBus(1-4)
flap_motor         = 0, 5 , 17.0
gear_motor         = 0, 5 , 17.0
autopilot          = 0, 5 , 17.0
avionics_bus       = 0, 10, 17.0
avionics           = 1, 5 , 17.0
pitot_heat         = 0, 2 , 17.0
additional_system  = 0, 20, 17.0
marker_beacon      = 1, 2 , 17.0
gear_warning       = 0, 2 , 17.0
fuel_pump          = 0, 5 , 17.0
starter1           = 0, 20, 17.0
light_nav          = 0, 5 , 17.0
light_beacon       = 0, 5 , 17.0
light_landing      = 0, 5 , 17.0
light_taxi         = 0, 5 , 17.0
light_strobe       = 0, 5 , 17.0
light_panel        = 0, 5 , 17.0

        //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, -15.900, 0.000, -3.100, 1500.000, 0.000, 0.500, 22.000, 0.250, 2.500, 0.700, 0.000, 0.000, 0.000, 0.000, 0.000
point.1 = 1.000, -1.100, -2.600, -5.700, 3500.000, 1.000, 0.500, 0.000, 0.300, 2.500, 0.700, 0.000, 0.000, 2.000, 0.000, 0.000
point.2 = 1.000, -1.100, 2.600, -5.700, 3500.000, 2.000, 0.500, 0.000, 0.300, 2.500, 0.700, 0.000, 0.000, 3.000, 0.000, 0.000
point.3 = 2.000, -3.900, -18.000, 3.000, 1800.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 5.000, 0.000, 0.000
point.4 = 2.000, -3.900, 18.000, 3.000, 1800.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 6.000, 0.000, 0.000
point.5= 2.000, -20.230, 0.000, 0.300, 1800.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 9.000, 0.000, 0.000
point.6= 2.000, 1.480, 0.000, -2.170, 1800.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 4.000, 0.000, 0.000
point.7= 2.000, -22.800, 0.000, 5.830, 1800.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 7.000, 0.000, 0.000
point.8= 2.000, -4.900, 0.000, -2.000, 1800.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 8.000, 0.000, 0.000

max_number_of_points = 21

static_pitch= 4.000
static_cg_height= 5.500

[Views]
eyepoint= -4.8,0,-0.8        //(feet) longitudinal, lateral, vertical distance from reference datum

[Radios]
// Radio Type = availiable, standby frequency, has glide slope
Audio.1       = 1
Com.1         = 1, 1
Com.2         = 1, 1
Nav.1         = 1, 1, 1
Nav.2         = 1, 1, 0
Adf.1         = 1
Transponder.1 = 1
Marker.1      = 1


               
[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 = 100,  180
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=1,0

[EFFECTS]
wake=fx_wake
water=fx_spray
dirt=fx_tchdrt
concrete=fx_sparks
touchdown=fx_tchdwn_s, 1

[fuel]
LeftMain  = -3.900, -2.100, 2.500, 26.500, 0.000
RightMain = -3.900, 2.100, 2.500, 26.500, 0.000
fuel_type = 1                                //Fuel type: 1 = Avgas, 2 = JetA
number_of_tank_selectors = 1                    

[airplane_geometry]
wing_area               = 174.000
wing_span               = 27.000
wing_root_chord         = 4.300
wing_dihedral           = 1.700
wing_incidence          = 1.500
wing_twist              = -3.000
oswald_efficiency_factor= 0.680
wing_winglets_flag      = 0
wing_sweep              = 0.000
wing_pos_apex_lon       = -2.400
wing_pos_apex_vert      = 0.000
htail_area              = 39.000
htail_span              = 11.700
htail_pos_lon           = -18.300
htail_pos_vert          = 0.000
htail_incidence         = 3.200
htail_sweep             = 10.000
vtail_area              = 18.000
vtail_span              = 4.800
vtail_sweep             = 40.000
vtail_pos_lon           = -16.200
vtail_pos_vert          = 1.500
elevator_area           = 16.600
aileron_area            = 18.300
rudder_area             = 6.700
elevator_up_limit       = 28.000
elevator_down_limit     = 21.000
aileron_up_limit        = 20.000
aileron_down_limit      = 15.000
rudder_limit            = 24.000
elevator_trim_limit     = 19.500
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




[Reference Speeds]
flaps_up_stall_speed    = 75.000	
full_flaps_stall_speed  = 75.000	
cruise_speed            = 120.000

[autopilot]
autopilot_available= 1
flight_director_available= 0
default_vertical_speed= 700.0
autothrottle_available= 0
pitch_takeoff_ga= 8.000

[forcefeedback]
gear_bump_nose_magnitude=6000           ; 0 - 10000
gear_bump_nose_direction=18000          ; 0 - 35999 degrees
gear_bump_nose_duration=250000          ; in microseconds
gear_bump_left_magnitude=6000           ; 0 - 10000
gear_bump_left_direction=35500          ; 0 - 35999 degrees
gear_bump_left_duration=250000          ; in microseconds
gear_bump_right_magnitude=6000          ; 0 - 10000
gear_bump_right_direction=00500         ; 0 - 35999 degrees
gear_bump_right_duration=250000         ; in microseconds
ground_bumps_magnitude1=3250            ; 0 - 10000
ground_bumps_angle1=8900                ; 0 - 35999 degrees
ground_bumps_intercept1=5.0
ground_bumps_slope1=0.48
ground_bumps_magnitude2=750             ; 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


[Flaps.0]
type= 0
span-outboard= 0.000
extending-time= 0.100
system_type= 0
damaging-speed= 0.000
blowout-speed= 0.000
lift_scalar= 0.000
drag_scalar= 0.000
pitch_scalar= 0.000