[fltsim.0]
title=SuperJet 100 Aeroproyecto Colors
sim=SSJ100
model=
panel=
sound=
texture=Aeroproyecto
kb_checklists=
kb_reference=
atc_id=CUB909
atc_id_color=
ui_manufacturer=AEROPROYECTO
ui_type="SUKHOI SuperJet SSJ-100"
ui_variation="Aeroproyecto Colors"
description="SUKHOI SuperJet 100 R1.1c FreeWare \nAEROPROYECTO 1999-2014 \nBy Edgar Guinart Lуpez\[email protected] \n\nFor more liveries and Paint Kit visit venesim.com"
visual_damage=1
[fltsim.1]
title=SuperJet 100 White Colors
sim=SSJ100
model=
panel=
sound=
texture=white
kb_checklists=
kb_reference=
atc_id=CUB909
atc_id_color=
ui_manufacturer=AEROPROYECTO
ui_type="SUKHOI SuperJet SSJ-100"
ui_variation="Work Templates Colors"
description="SUKHOI SuperJet 100 R1.1c FreeWare \nAEROPROYECTO 1999-2014 \nBy Edgar Guinart Lуpez\[email protected] \n\nFor more liveries and Paint Kit visit venesim.com"
visual_damage=1
[fltsim.2]
title=SuperJet 100 SimuCuba Colors
sim=SSJ100
model=
panel=
sound=
texture=SimuCuba
kb_checklists=
kb_reference=
atc_id=CUB909
atc_id_color=
ui_manufacturer=AEROPROYECTO
ui_type="SUKHOI SuperJet SSJ-100"
ui_variation="SimuCuba Colors"
description="SUKHOI SuperJet 100 R1.1c FreeWare \nAEROPROYECTO 1999-2014 \nBy Edgar Guinart Lуpez\[email protected] \n\nFor more liveries and Paint Kit visit venesim.com"
visual_damage=1
//Please, donґt edit behind this point, the dynamics can be seriously damage!
[General]
atc_type=SUKHOI
atc_model=SuperJet
editable=0
performance="Velocidad de crucero: 477 nudos (885 km\/h) \nMotores: SAM-146 with 17,270 lbs max thrust \nAlcance mбximo: 2390 mn (4420 km) \nTecho de servicio: 41000 pies (12500 m) \nCapacidad de combustible: 3500 U.S. galons (10681 kg) \nPeso en vacнo: 55000 lb (25000 kg) \nPeso bruto mбximo: 105000 lbs (47727 kg) \nLargo: 98,23 pies (29,94 m) \nEnvergadura: 91,20 pies (27,8 m) \nAlto: 33,73 pies (10,28 m) \nPlazas: Asientos 98 (Standard single class) \nCapacidad de carga: 775,8 pies3 (21,97 m3)"
[pitot_static]
vertical_speed_time_constant = 999 //Increasing this value will cause a more instantaneous reaction in the VSI
[WEIGHT_AND_BALANCE]
max_gross_weight = 105000 // (pounds)
empty_weight = 55000 // (pounds) *** 55000 lbs Empty Weight (EW)
reference_datum_position = 0, 0, 0 // (feet) distance from FlightSim Reference position: (1/4 chord, centerline, waterline)
empty_weight_CG_position = 3.0, 0.0, -3.6 // (feet) longitudinal, lateral, vertical distance from specified datum
max_number_of_stations = 50
//Weight (lbs), longitudinal, lateral, vertical positions from datum (feet) *** Tipical conf.: 15488 lbs pax, 800 lbs F-bag and 2200 lbs R-bag
station_load.0 = "4000, 18.7, 0.0, 0.0, 23 Pax 5060 lbs Max"
station_load.1 = "4000, 6.0, 0.0, 0.0, 25 Pax 5500 lbs Max"
station_load.2 = "4000, -6.6, 0.0, 0.0, 25 Pax 5500 lbs Max"
station_load.3 = "4000, -19.3, 0.0, 0.0, 25 Pax 5500 lbs Max"
station_load.4 = "1000, 24.0, 0.0, -4.6, Bag 3180 lbs Max"
station_load.5 = "1000, -22.0, 0.0, -4.6, Bag 4960 lbs Max"
;Moments of Inertia
empty_weight_pitch_MOI =652000 // 652000
empty_weight_roll_MOI =243000 // 243000
empty_weight_yaw_MOI =637000 // 637000
empty_weight_coupled_MOI=0
CG_forward_limit=0.0
CG_aft_limit=1.0
[fuel]
Center1 = 4.0, 0, -3.3, 440, 0 // 1473 LR - 440 BASIC //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)
LeftMain = -1.9, -19, -2.6, 1351, 0 //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)
RightMain = -1.9, 19, -2.6, 1351, 0 //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)
fuel_type = 2 //Fuel type: 1 = Avgas, 2 = JetA
number_of_tank_selectors = 2
electric_pump=1
[GeneralEngineData]
engine_type = 1 //0=Piston, 1=Jet, 2=None, 3=Helo-Turbine, 4=Rocket, 5=Turboprop
Engine.0 = 0.0, -14.9, -6.9 //(feet) longitudinal, lateral, vertical distance from reference datum *** 0.0, -14.9, -6.9
Engine.1 = 0.0, 14.9, -6.9 //(feet) longitudinal, lateral, vertical distance from reference datum *** 0.0, 14.9, -6.9
fuel_flow_scalar = 0.93 //Scalar for fuel flow efficiency
min_throttle_limit = -0.50 //Minimum percent throttle. Generally negative for turbine reverser
max_contrail_temperature = -30 //Temperature (deg C) below which contrails may appear
[TurbineEngineData]
fuel_flow_gain = 0.002 //Gain on fuel flow
inlet_area = 12.56 //Square Feet, engine nacelle inlet area *** FAN = 12.56 sf
rated_N2_rpm = 18523 //RPM, second stage compressor rated value
static_thrust = 17270 //Lbs, max rated static thrust at Sea Level *** Max = 17270 lbf
afterburner_available = 0 //Afterburner available?
reverser_available = 1 //Thrust reverser available?
[jet_engine]
thrust_scalar = 1.0
[electrical]
;BusType, MaxAmpLoad, MinVoltage BusTypes:0=MainBus,1=AvionicsBus,2=BatteryBus,3=HotBatteryBus,4-7=Generator/AlternatorBus(1-4)
max_battery_voltage =28.0
generator_alternator_voltate =30.0
max_generator_alternator_amps =200.0
flap_motor = 0, 0 , 17.0
gear_motor = 0, 0 , 17.0
autopilot = 0, 0 , 17.0
avionics_bus = 0, 0 , 17.0
avionics = 1, 0 , 17.0
pitot_heat = 0, 0 , 17.0
additional_system = 0, 0 , 17.0
marker_beacon = 1, 0 , 17.0
gear_warning = 0, 0 , 17.0
fuel_pump = 0, 0 , 17.0
starter1 = 0, 0 , 17.0
starter2 = 0, 0 , 17.0
light_nav = 0, 0 , 17.0
light_beacon = 0, 0 , 17.0
light_strobe = 0, 0 , 17.0
light_landing = 0, 0 , 17.0
light_taxi = 0, 0 , 17.0
light_panel = 0, 0 , 17.0
light_cabin = 0, 0 , 17.0
light_recognition = 0, 0 , 17.0
light_wing = 0, 0 , 17.0
light_logo = 0, 0 , 17.0
auto_brakes = 0, 0 , 17.0
standby_vacuum = 0, 0 , 17.0
hydraulic_pump = 0, 0 , 17.0
fuel_transfer_pump = 0, 0 , 17.0
propeller_deice = 0, 0 , 17.0
directional_gyro = 0, 0 , 17.0
directional_gyro_slaving = 0, 0 , 17.0
//0 Class <0=none,1=wheel, 2=scrape, 3=float>
//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
//14 Airspeed limit for retraction (KIAS)
//15 Airspeed that gear gets damage at (KIAS)
[contact_points]
point.0=1, 33.70, 0.00, -11.80, 1181.1, 0, 1.0, 65.00, 0.6, 2.0, 0.5, 4.0, 4.0, 0, 216.0, 256.0
point.1=1, -3.00, -9.20, -11.80, 1574.8, 1, 1.5, 0.00, 0.6, 1.5, 0.5, 7.0, 7.0, 2, 216.0, 256.0
point.2=1, -3.00, 9.20, -11.80, 1574.8, 2, 1.5, 0.00, 0.6, 1.5, 0.5, 7.0, 7.0, 3, 216.0, 256.0
// Hard countach
point.3 = 2, 10.0, -14.90, -10.00, 1600, 0, 0.00, 0.0, 0.3, 2.5, 0.6, 0.0, 0.0, 7, 0.0, 0.0
point.4 = 2, 10.0, 14.90, -10.00, 1600, 0, 0.00, 0.0, 0.3, 2.5, 0.6, 0.0, 0.0, 7, 0.0, 0.0
point.5 = 2, 34.00, 0.00, -6.00, 1600, 0, 0.00, 0.0, 0.5, 2.5, 0.5, 0.0, 0.0, 7, 0.0, 0.0
point.6 = 2, -25.00, 0.00, -6.00, 1600, 0, 0.00, 0.0, 0.5, 2.5, 0.5, 0.0, 0.0, 7, 0.0, 0.0
// crash points
point.7 =2, -11.60, -45.00, 0.00, 515, 0, 0.0, 0.0, 0.00, 0.0, 0.0, 0.0, 0.0, 5, 0.0, 0.0
point.8 =2, -11.60, 45.00, 0.00, 515, 0, 0.0, 0.0, 0.00, 0.0, 0.0, 0.0, 0.0, 6, 0.0, 0.0
point.9 =2, 40.00, 0.00, -3.00, 920, 0, 0.0, 0.0, 0.00, 0.0, 0.0, 0.0, 0.0, 9, 0.0, 0.0
point.10=2, -51.00, 0.00, 0.00, 920, 0, 0.0, 0.0, 0.00, 0.0, 0.0, 0.0, 0.0, 4, 0.0, 0.0
max_number_of_points = 21
static_pitch=0.00 //degrees, pitch when at rest on the ground (+=Up, -=Dn)
static_cg_height=11.90 //feet, altitude of CG when at rest on the ground
gear_system_type=1 //Hydraulic
[gear_warning_system]
gear_warning_available = 1 //Normal
pct_throttle_limit = 0.1 //Percent throttle that activates warning
flap_limit_idle = 9.0 //Flap angle that activates warning at idle
flap_limit_power = 25.0 //Flap angle that activates warning at above idle
[brakes]
parking_brake = 1 //Parking brake available
toe_brakes_scale = 0.8 //Brake scalar
[hydraulic_system]
normal_pressure = 3000.0 //PSI
electric_pumps = 1 //no electric pumps
engine_map = 1,1,0,0 //pumps on Eng1,2
[Views]
eyepoint=36.3, -1.85, 1.8 //(feet) longitudinal, lateral, vertical distance from reference datum
[flaps.0] //Trailing Edge Flaps
type = 1 // 1 - tail, 2 - lead
span-outboard = 0.7 // 0.0 .. 1.0
extending-time = 20 // seconds
flaps-position.0 = 0 // degrees
flaps-position.1 = 3 // degrees
flaps-position.2 = 9 // degrees
flaps-position.3 = 16 // degrees
flaps-position.4 = 25 // degrees
flaps-position.5 = 36 // degrees
damaging-speed = 260 // KIAS
blowout-speed = 308 // KIAS
lift_scalar = 1.0
drag_scalar = 1.0
pitch_scalar= 1.0
system_type = 1 //Hydraulic
[flaps.1] //Leading Edge Slats
type = 2 // 1 - tail, 2 - lead
span-outboard = 0.9 // 0.0 .. 1.0
extending-time = 10 // seconds
flaps-position.0 = 0 // degrees
flaps-position.1 = 18.0 // degrees
flaps-position.2 = 18.0 // degrees
flaps-position.3 = 24.0 // degrees
damaging-speed = 260 // KIAS
blowout-speed = 308 // KIAS
lift_scalar = 1.0
drag_scalar = 1.0
pitch_scalar= 1.0
system_type = 1 //Hydraulic
[Radios]
// Radio Type = availiable, standby frequency, has glide slope
Audio.1 = 1
Com.1 = 1, 0
Com.2 = 1, 1
Nav.1 = 1, 1, 1
Nav.2 = 1, 1, 0
Adf.1 = 1, 0
Adf.2 = 1, 0
Transponder.1 = 1
Marker.1 = 1
[LIGHTS]
//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing
light.0 = 3, -11.50, -44.90, 0.51, fx_navredm ,
light.1 = 3, -11.50, 44.90, 0.51, fx_navgrem ,
light.2 = 2, -50.50, 0.00, 22.50, fx_strobeh ,
light.3 = 2, -11.60, -45.00, 0.51, fx_strobeh ,
light.4 = 2, -11.60, 45.00, 0.51, fx_strobeh ,
light.5 = 1, 3.20, -0.75, -6.90, fx_beaconb ,
light.6 = 1, 3.65, 0.00, 5.76, fx_beaconh ,
light.7 = 4, 35.20, 0.00, 2.88, fx_vclighth ,
light.8 = 5, 10.40, -6.20, -3.30, fx_landing ,
light.9 = 5, 10.40, 6.20, -3.30, fx_landing ,
light.10 = 7, 10.60, -5.70, -3.25, fx_landing ,
light.11 = 7, 10.60, 5.70, -3.25, fx_landing ,
light.12= 6, 34.70, -0.55, -8.35, fx_landing ,
light.13= 6, 34.70, 0.55, -8.35, fx_landing ,
light.14 = 3, -16.10, -45.70, 0.60, fx_navwhi ,
light.15 = 3, -16.10, 45.70, 0.60, fx_navwhi ,
light.16=9, 34.80, -0.25, -8.70, fx_landing ,
light.17=9, 34.80, 0.25, -8.70, fx_landing ,
[EFFECTS]
wake=fx_wake
water=fx_spray
dirt=fx_tchdrt
concrete=fx_sparks
touchdown=fx_tchdwn, 1
[SMOKESYSTEM]
smoke.0= 0.00, -15.5, -45.5, SSJ100_vortex
smoke.1= 0.00, -15.5, 45.5, SSJ100_vortex
[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 = 150, 250
aileron = 150, 250
rudder = 150, 250
[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=3,0
[attitude_indicators]
//Type: 0=None, 1=Vacuum Gyro, 2=Electric Gyro
attitude_indicator.0 = 1
[turn_indicators]
//Type: 0=None, 1=Electric Gyro, 2= Vacuum Gyro
turn_indicator.0=0,0
[exits]
number_of_exits = 2
exit_rate.0 = 0.3 ;Percent per second
exit_rate.1 = 0.3 ;Percent per second
[autopilot]
autopilot_available=1
flight_director_available=1
default_vertical_speed=1800
autothrottle_available=1
autothrottle_arming_required=1
autothrottle_max_rpm = 99
autothrottle_takeoff_ga=1
pitch_takeoff_ga = 8
max_pitch=10.0
max_pitch_acceleration=0.8
max_pitch_velocity_lo_alt=1.0
max_pitch_velocity_hi_alt=1.0
max_pitch_velocity_lo_alt_breakpoint=20000.0
max_pitch_velocity_hi_alt_breakpoint=28000.0
max_bank=25.0
max_bank_acceleration=3.0
max_bank_velocity=3.00
max_throttle_rate=0.1
nav_proportional_control=9.00
nav_integrator_control=0.25
nav_derivative_control=0.00
nav_integrator_boundary=2.50
nav_derivative_boundary=0.00
gs_proportional_control=19.0
gs_integrator_control=0.53
gs_derivative_control=0.00
gs_integrator_boundary=0.70
gs_derivative_boundary=0.00
yaw_damper_gain = 1.0
[flight_tuning]
cruise_lift_scalar = 1.0
parasite_drag_scalar = 1.0
induced_drag_scalar = 1.0
elevator_effectiveness = 1.0
aileron_effectiveness = 1.0
rudder_effectiveness = 1.0
pitch_stability = 1.0
roll_stability = 1.0
yaw_stability = 1.0
elevator_trim_effectiveness = 1.3
aileron_trim_effectiveness = 1.3
rudder_trim_effectiveness = 1.0
hi_alpha_on_roll=1.0
hi_alpha_on_yaw=1.0
[airplane_geometry]
wing_area = 829 //Square feet *** 829 wings *** 212 between wings root
wing_span = 91.21 //Feet
wing_root_chord = 17.7 //Feet
wing_dihedral = 6.0 //Degrees
wing_incidence = 1.5 //Degrees
wing_twist = -1.0 //Degrees
oswald_efficiency_factor= 0.9 //Measure of lift effeciency of wing
wing_winglets_flag = 0 //Are winglets available?
wing_sweep = 28.7 //Degrees, wing leading edge
wing_pos_apex_lon = 13.5 //Feet, longitudinal distance from reference point, negative going aft
wing_pos_apex_vert = -3.6 //Feet, vertical distance from reference point, positive going up
htail_area = 213.0 //Square feet
htail_span = 34.0 //Feet
htail_pos_lon = -37.1 //Feet, longitudinal distance from reference point, negative going aft
htail_pos_vert = 2.0 //Feet, vertical distance from reference point, positive going up
htail_incidence = -3.0 //Degrees
htail_sweep = 34.0 //Degrees, horizontal tail leading edge
vtail_area = 165.0 //Square feet
vtail_span = 17.25 //Feet, tip to body
vtail_sweep = 40.0 //Degrees, vertical tail leading edge
vtail_pos_lon = -30.6 //Feet, longitudinal distance from reference point, negative going aft
vtail_pos_vert = 5.0 //Feet, vertical distance from reference point, positive going up
elevator_area = 70.5 //Square feet
aileron_area = 26.9 //Square feet
rudder_area = 56.2 //Square feet
elevator_up_limit = 22.5 //Degrees
elevator_down_limit = 19.5 //Degrees
aileron_up_limit = 20.0 //Degrees
aileron_down_limit = 20.0 //Degrees
rudder_limit = 26.0 //Degrees
elevator_trim_limit = 16.0 //Degrees
spoiler_limit = 60.0 //Degrees
spoilerons_available = 1 //Spoilerons Available?
aileron_to_spoileron_gain = 3 //Aileron to spoileron gain
min_ailerons_for_spoilerons = 10 //Degrees
min_flaps_for_spoilerons = 0 //Minimum flap handle position when spoilerons activate
[Reference Speeds]
flaps_up_stall_speed = 110.0 //Knots True (KTAS)
full_flaps_stall_speed = 95.0 //Knots True (KTAS)
cruise_speed = 460.0 //Knots True (KTAS)
max_mach = 0.88 //Max Mach
max_indicated_speed = 356 //Red line (KIAS)
[stall_warning]
type=2
[forcefeedback]
gear_bump_nose_magnitude=3000 ; 0 - 10000
gear_bump_nose_direction=18000 ; 0 - 35999 degrees
gear_bump_nose_duration=250000 ; in microseconds
gear_bump_left_magnitude=2700 ; 0 - 10000
gear_bump_left_direction=35500 ; 0 - 35999 degrees
gear_bump_left_duration=250000 ; in microseconds
gear_bump_right_magnitude=2700 ; 0 - 10000
gear_bump_right_direction=00500 ; 0 - 35999 degrees
gear_bump_right_duration=250000 ; in microseconds
ground_bumps_magnitude1=1300 ; 0 - 10000
ground_bumps_angle1=08900 ; 0 - 35999 degrees
ground_bumps_intercept1=3.0
ground_bumps_slope1=0.20
ground_bumps_magnitude2=200 ; 0 - 10000
ground_bumps_angle2=09100 ; 0 - 35999 degrees
ground_bumps_intercept2=1.075
ground_bumps_slope2=0.035
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 microse