[fltsim.0]
title=Aviat Pitts Special S1 T
sim=Pitts S1T
model=
panel=
sound=
texture=
kb_reference=Specs
kb_checklists=Checklist
ui_manufacturer=Aviat
ui_type=Pitts Special
ui_variation=S1-T
atc_id=ZSMZX
description=The original prototype of the S1 Special first flew in September 1944. The designer of the original Pitts Special aerobatic biplane, Curtiss Pitts, could hardly have appreciated that his design would continue in production for over five decades, and that it would come to be considered by the general public as the definitive aerobatic and display flying aircraft.\nThe S1T was introduced to production in 1981, and introduced a 150kW (200hp) Lycoming (now Textron Lycoming) AEIO360 driving a constant speed prop, symmetrical wings and four ailerons.\nThis aircraft includes a custom-designed panel, full lighting effects, opening canopy, full animation, reflective textures and two-color multiple smoke system. \n\n\n
atc_heavy=0
atc_airline=
atc_flight_number=
[fltsim.1]
title=Aviat Pitts Special S1 T Paint1
sim=Pitts S1T
model=
panel=
sound=
texture=1
kb_reference=Specs
kb_checklists=Checklist
ui_manufacturer=Aviat
ui_type=Pitts Special
ui_variation=S1-T
atc_id=ZSMZX
description=The original prototype of the S1 Special first flew in September 1944. The designer of the original Pitts Special aerobatic biplane, Curtiss Pitts, could hardly have appreciated that his design would continue in production for over five decades, and that it would come to be considered by the general public as the definitive aerobatic and display flying aircraft.\nThe S1T was introduced to production in 1981, and introduced a 150kW (200hp) Lycoming (now Textron Lycoming) AEIO360 driving a constant speed prop, symmetrical wings and four ailerons.\nThis aircraft includes a custom-designed panel, full lighting effects, opening canopy, full animation, reflective textures and two-color multiple smoke system. \n\n\n
atc_heavy=0
atc_airline=
atc_flight_number=
[fltsim.2]
title=Aviat Pitts Special S1 T Paint2
sim=Pitts S1T
model=
panel=
sound=
texture=2
kb_reference=Specs
kb_checklists=Checklist
ui_manufacturer=Aviat
ui_type=Pitts Special
ui_variation=S1-T
atc_id=ZSMZX
description=The original prototype of the S1 Special first flew in September 1944. The designer of the original Pitts Special aerobatic biplane, Curtiss Pitts, could hardly have appreciated that his design would continue in production for over five decades, and that it would come to be considered by the general public as the definitive aerobatic and display flying aircraft.\nThe S1T was introduced to production in 1981, and introduced a 150kW (200hp) Lycoming (now Textron Lycoming) AEIO360 driving a constant speed prop, symmetrical wings and four ailerons.\nThis aircraft includes a custom-designed panel, full lighting effects, opening canopy, full animation, reflective textures and two-color multiple smoke system. \n\n\n
atc_heavy=0
atc_airline=
atc_flight_number=
[fltsim.3]
title=Aviat Pitts Special S1 T Paint3
sim=Pitts S1T
model=
panel=
sound=
texture=3
kb_reference=Specs
kb_checklists=Checklist
ui_manufacturer=Aviat
ui_type=Pitts Special
ui_variation=S1-T
atc_id=ZSMZX
description=The original prototype of the S1 Special first flew in September 1944. The designer of the original Pitts Special aerobatic biplane, Curtiss Pitts, could hardly have appreciated that his design would continue in production for over five decades, and that it would come to be considered by the general public as the definitive aerobatic and display flying aircraft.\nThe S1T was introduced to production in 1981, and introduced a 150kW (200hp) Lycoming (now Textron Lycoming) AEIO360 driving a constant speed prop, symmetrical wings and four ailerons.\nThis aircraft includes a custom-designed panel, full lighting effects, opening canopy, full animation, reflective textures and two-color multiple smoke system. \n\n\n
atc_heavy=0
atc_airline=
atc_flight_number=
[General]
atc_type=PITTS
atc_model=PTS1
performance=Length: \t 15ft 6in\nHeight: \t 6ft 3in\nWing span: 17ft 4in\nWing area: 98.5sq ft\nWeight - empty: 720lb\n - MTOW: 1150lb\nPowerplant: Textron Lycoming AEIO360 Propeller: Constant speed\nMaximum sped: 153kt\nCruise speed: 123kt\nNever exceed speed: 199 kt\nRange: \t\t 275nm (no reserve)\nCeiling: \t\t 22,300ft\n
Category=airplane
[WEIGHT_AND_BALANCE]
max_gross_weight = 1150.000
empty_weight = 720.000
reference_datum_position = 0.000, 0.000, 0.000
empty_weight_CG_position = 0.000, 0.000, 0.000
max_number_of_stations = 50
station_load.0 = "170.000, -1.000, 0.000, 0.000, Pilot"
;Moments of Inertia
empty_weight_pitch_MOI = 1417.000
empty_weight_roll_MOI = 900.000
empty_weight_yaw_MOI = 1656.000
empty_weight_coupled_MOI = 0.000
CG_forward_limit= 0.000
CG_aft_limit= 1.000
[electrical]
max_battery_voltage = 12.0
generator_alternator_voltage = 13.8
max_generator_alternator_amps = 40.0
;BusType, MaxAmpLoad, MinVoltage BusTypes:0=MainBus,1=AvionicsBus,2=BatteryBus,3=HotBatteryBus,4-7=Generator/AlternatorBus(1-4)
avionics_bus = 0, 10, 9.5
avionics = 1, 5 , 9.5
additional_system = 0, 20, 9.5
marker_beacon = 1, 2 , 9.0
fuel_pump = 0, 5 , 9.0
[flight_tuning]
cruise_lift_scalar =1.000
parasite_drag_scalar =0.836
induced_drag_scalar =1.000
elevator_effectiveness =2.000
aileron_effectiveness =1.500
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 = 2.000, 0.000, 0.000
fuel_flow_scalar= 1.933
min_throttle_limit=0.000000
[piston_engine]
power_scalar =1.000
cylinder_displacement= 90.300
compression_ratio= 8.700
number_of_cylinders= 4
max_rated_rpm= 2850.000
max_rated_hp= 200.000
fuel_metering_type= 0
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= 0
propeller_diameter= 6.200
propeller_blades= 3
propeller_moi= 5.900
beta_max= 34.000
beta_min= 17.000
min_gov_rpm= 1400.000
prop_tc= 0.100
gear_reduction_ratio= 1.000
fixed_pitch_beta= 0.000
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
//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, -9.400, 0.000, -1.200, 1377.950, 0.000, 0.160, 180.000, 0.350, 2.500, 0.700, 0.000, 0.000, 0.000, 0.000, 0.000
point.1= 1.000, 1.600, -2.100, -3.000, 1968.500, 1.000, 0.550, 0.000, 0.300, 2.000, 0.700, 0.000, 0.000, 2.000, 0.000, 0.000
point.2= 1.000, 1.600, 2.100, -3.000, 1968.500, 2.000, 0.550, 0.000, 0.300, 2.000, 0.700, 0.000, 0.000, 3.000, 0.000, 0.000
point.3= 2.000, 0.000, -8.700, 3.000, 787.400, 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, 0.000, 8.700, 3.000, 787.400, 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, -9.900, 0.000, 1.300, 787.400, 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, 5.500, 0.000, 1.200, 787.400, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 4.000, 0.000, 0.000
static_pitch = 11.300
static_cg_height = 2.790
point.7= 2.000, -0.800, -8.500, 0.200, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 5.000, 0.000, 0.000
point.8= 2.000, -0.800, 8.500, 0.200, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 6.000, 0.000, 0.000
[Views]
eyepoint=-1.60,0.000000,2.45
[Radios]
// Radio Type = availiable, standby frequency, has glide slope
Audio.1 = 1
Com.1 = 1, 1
Nav.1 = 1, 1, 1
Transponder.1 = 1
[SMOKESYSTEM]
smoke.0=-0.8,0.00, -8.4, fx_smoke_r
smoke.1=-0.8,0.00, 8.4, fx_smoke_r
smoke.2=-1.6, 0.00, 0.00, fx_smoke_w
[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 = 140, 240
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
[LIGHTS]
//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing
light.0=3, 0.50,-7.79, 0.31, fx_navredm ,
light.1=3, 0.50, 7.79, 0.31, fx_navgrem ,
light.2=3, 1.24,-8.02, 3.09, fx_navredm ,
light.3=3, 1.24, 8.02, 3.09, fx_navgrem ,
light.4=2, -0.80,-8.66, 0.26, fx_strobeh ,
light.5=2, -0.80,8.66, 0.26, fx_strobeh ,
light.6=2, -0.10,-8.78, 3.03, fx_strobeh ,
light.7=2, -0.10,8.78, 3.03, fx_strobeh ,
light.8=4, -0.30, 0.00, 2.20, fx_vclight ,
[EFFECTS]
wake=fx_wake
water=fx_spray
dirt=fx_tchdrt
concrete=fx_sparks
touchdown=fx_tchdwn_s, 1
[fuel]
Center1= 0.000, 0.000, 0.000, 35.000, 0.000
LeftAux= 0.000, 0.000, 0.0, 0.0, 0.000
RightAux= 0.000, 0.000,0.0, 0.0, 0.000
fuel_type=1.000000
number_of_tank_selectors=1
electric_pump=1
[airplane_geometry]
wing_area = 98.500
wing_span = 17.400
wing_root_chord = 4.750
wing_dihedral = 2.000
wing_incidence = 0.698
wing_twist = 0.500
oswald_efficiency_factor= 0.847
wing_winglets_flag = 0
wing_sweep = 0.000
wing_pos_apex_lon = -1.000
wing_pos_apex_vert = 0.000
htail_area = 28.000
htail_span = 10.500
htail_pos_lon = -13.100
htail_pos_vert = 0.000
htail_incidence = 0.000
htail_sweep = 10.000
vtail_area = 15.000
vtail_span = 4.400
vtail_sweep = 20.000
vtail_pos_lon = -14.300
vtail_pos_vert = 1.500
elevator_area = 10.000
aileron_area = 18.000
rudder_area = 7.000
elevator_up_limit = 26.000
elevator_down_limit = 26.000
aileron_up_limit = 30.000
aileron_down_limit = 30.000
rudder_limit = 30.000
elevator_trim_limit = 15.000
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
auto_spoiler_available=0
positive_g_limit_flaps_up=10.000000
positive_g_limit_flaps_down=10.000000
negative_g_limit_flaps_up=-10.000000
negative_g_limit_flaps_down=-10.000000
[Reference Speeds]
flaps_up_stall_speed = 55.000
full_flaps_stall_speed = 55.000
cruise_speed = 123.000
max_indicated_speed=200.000000
[autopilot]
autopilot_available=0
flight_director_available=0
[forcefeedback]
ground_bumps_magnitude1=3000 ; 0 - 10000
ground_bumps_angle1=8900 ; 0 - 35999 degrees
ground_bumps_intercept1=4.0
ground_bumps_slope1=0.25
ground_bumps_magnitude2=350 ; 0 - 10000
ground_bumps_angle2=9100 ; 0 - 35999 degrees
ground_bumps_intercept2=0.075
ground_bumps_slope2=0.7
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
[brakes]
toe_brakes_scale=0.824000
parking_brake=1
[hydraulic_system]
normal_pressure=0.000000
[stall_warning]
type=1
stick_shaker=0
[attitude_indicators]
attitude_indicator.0=1
[turn_indicators]
turn_indicator.0=1,0
[Flaps.0]
type= 0
span-outboard= 0.125
extending-time= 5.000
system_type= 4
damaging-speed= 0.000
blowout-speed= 0.000
lift_scalar= 1.000
drag_scalar= 1.000
pitch_scalar= 1.000
[pitot_static]
pitot_heat=0.000000
[vacuum_system]
max_pressure=5.150000
vacuum_type=1
electric_backup_pressure=0.000000
engine_map=1,0,0,0
[pneumatic_system]
max_pressure=0.000000
bleed_air_scalar=1.000000
[deice_system]
structural_deice_type=0
