[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.\ngilles_arlove@yahoo.com
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.\ngilles_arlove@yahoo.com
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
