[fltsim.0]
title=Tu-104SH
sim=Tu104
model=sh
panel=
sound=
texture=2
checklists=
kb_checklists=
kb_reference=
atc_id=42342
atc_airline=Af
atc_flight_number=
editable=1
ui_manufacturer=Tupolev
ui_type=Tu-104
ui_variation=Nav Trainer
visual_damage=0
description=flight dynamic ver. 1.0 by Oleg Tchernikov. For Tu-104A only.
atc_heavy=0

[General]
performance=\n
atc_type=TUPOLEV
atc_model=TU104

[WEIGHT_AND_BALANCE]
max_gross_weight= 167548.500
empty_weight= 95458.000
reference_datum_position= 0.000, 0.000, 0.000
empty_weight_CG_position= 0.000, 0.000, 0.000
max_number_of_stations=3

station_load.0=250.000, 0.000, 0.000, 0.000
station_load.1=2000.000, 0.000, 0.000, 0.000
station_load.2=1000.000, 0.000, 0.000, 0.000


;Moments of Inertia
empty_weight_roll_MOI= 2262183.000
empty_weight_pitch_MOI= 3172439.000
empty_weight_yaw_MOI= 3337024.000
empty_weight_coupled_MOI= 1000.000
CG_forward_limit= 0.000
CG_aft_limit= 1.000
reference_datum_position=0.000000,0.000000,0.000000



[GeneralEngineData]
engine_type= 1
fuel_flow_scalar = 1.226
Engine.0= -1.667, -4.000, -1.000
Engine.1= -1.667, 4.000, -1.000
min_throttle_limit=-0.250000
max_contrail_temperature=-27

[TurbineEngineData]
fuel_flow_gain= 0.002
inlet_area= 10.170
rated_N2_rpm= 4900.000
static_thrust= 20943.000
afterburner_available= 0
reverser_available= 0

[jet_engine]
thrust_scalar = 1.000

[fuel]
number_of_tank_selectors = 2
electric_pump = 1
Center1 = 1.26, 0, 0, 1151.7, 0
LeftAux = -8, -26.5, 0, 393.27, 0
LeftTip = -15, -34.5, 0, 125, 0
RightAux = -8, 26.5, 0, 393.27, 0
RightTip = -15, 34.5, 0, 125, 0
External1 = 0, -11.6, 0, 633.43, 0
External2 = 0, 11.6, 0, 633.43, 0
fuel_type=2.000000

[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 = 1.25
aileron_trim_effectiveness  = 1.0
rudder_trim_effectiveness   = 1.0

[Views]
eyepoint=37.729659,-1.307210,3.614050

[Flaps.0]
type= 1
span-outboard= 0.600
extending-time= 12.000
system_type= 0
damaging-speed= 210.000
blowout-speed= 230.000
lift_scalar= 1.000
drag_scalar= 1.000
pitch_scalar= 1.000
flaps-position.0= 0.000, 0.000
flaps-position.1= 10.000, 0.000
flaps-position.2= 15.000, 0.000
flaps-position.3= 20.000, 0.000
flaps-position.4= 35.000, 0.000

[electrical]
max_battery_voltage = 24
generator_alternator_voltage = 28
max_generator_alternator_amps = 60
engine_generator_map = 1,1
electric_always_available = 0
flap_motor = 0, 5, 17
gear_motor = 0, 5, 17
autopilot = 0, 5, 17
avionics_bus = 0, 5, 17
avionics = 1, 5, 17
pitot_heat = 0, 2, 17
additional_system = 0, 2, 17
marker_beacon = 1, 2, 17
gear_warning = 0, 2, 17
fuel_pump = 0, 5, 17
starter1 = 0, 20, 17
light_nav = 0, 5, 17
light_beacon = 0, 5, 17
light_landing = 0, 5, 17
light_taxi = 0, 5, 17
light_strobe = 0, 5, 17
light_panel = 0, 5, 17

[airplane_geometry]
wing_area= 1872.000
wing_span= 113.600
wing_root_chord= 24.600
wing_dihedral= 2.000
wing_incidence= 1.000
wing_twist= -3.000
oswald_efficiency_factor= 0.981
wing_winglets_flag= 0
wing_sweep= 35.000
wing_pos_apex_lon= 0.000
wing_pos_apex_vert= -3.000
htail_area= 448.000
htail_span= 43.960
htail_pos_lon= -49.000
htail_pos_vert= 0.000
htail_incidence= 0.000
htail_sweep= -40.000
vtail_area= 253.280
vtail_span= 19.840
vtail_sweep= -45.000
vtail_pos_lon= -42.000
vtail_pos_vert= 14.167
elevator_area= 68.980
aileron_area= 80.520
rudder_area= 61.920
elevator_up_limit= 20.000
elevator_down_limit= 12.000
aileron_up_limit= 19.500
aileron_down_limit= 14.500
rudder_limit= 25.000
elevator_trim_limit= 20.500
spoiler_limit= 35.000
spoilerons_available= 0
aileron_to_spoileron_gain= 3.000
min_ailerons_for_spoilerons= 10.000
min_flaps_for_spoilerons= 0.000

[contact_points]
point.0= 1.000, 40.000, 0.000, -11.5, 1181.102, 0.000, 1.445, 45.0, 1.003, 2.500, 0.799, 10.000, 15.000, 0.000, 190.000, 232.000
point.1= 1.000, -4.750, -19.0, -11.7, 1574.803, 1.000, 1.445, 0.000, 1.003, 2.500, 0.699, 16.900, 12.900, 2.000, 240.000, 240.000
point.2= 1.000, -4.750, 19.0, -11.7, 1574.803, 2.000, 1.445, 0.000, 1.003, 2.500, 0.699, 17.100, 13.100, 3.000, 240.000, 248.000
point.3= 2.000, -14.167, -47.333, 0.000, 787.402, 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, -14.167, 47.333, 0.000, 787.402, 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, -54.000, 0.000, 2.833, 787.402, 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, 42.667, 0.000, -3.750, 787.402, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 4.000, 0.000, 0.000
static_pitch= 0.390
static_cg_height= 7.791
gear_system_type=0

[keyboard_response]
elevator=150.000000,250.000000
aileron=150.000000,250.000000
rudder=150.000000,250.000000

[autopilot]
autopilot_available=1 
flight_director_available=1 
default_vertical_speed=1800 
autothrottle_available=1 
autothrottle_arming_required=1
autothrottle_max_rpm = 90
autothrottle_takeoff_ga=1
pitch_takeoff_ga=7 ;
max_pitch=12.0
max_pitch_acceleration=1.0
max_pitch_velocity_lo_alt=2.0
max_pitch_velocity_hi_alt=1.5
max_pitch_velocity_lo_alt_breakpoint=20000.0
max_pitch_velocity_hi_alt_breakpoint=28000.0
max_bank=25.0
max_bank_acceleration=1.8
max_bank_velocity=3.00
max_throttle_rate=0.10
nav_proportional_control=12.00
nav_integrator_control=0.25
nav_derivative_control=0.00
nav_integrator_boundary=2.50
nav_derivative_boundary=0.00
gs_proportional_control=25.0
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

[Reference Speeds]
flaps_up_stall_speed= 190.000
full_flaps_stall_speed= 121.500
cruise_speed=442.700
max_indicated_speed=325.000000
max_mach=0.859961

[Radios]
Audio.1=1
Com.1=1, 0
Com.2=1, 0
Nav.1=1, 0, 1
Nav.2=1, 0, 0
Adf.1=1
Adf.2=1
Transponder.1=1
Marker.1=1 

[LIGHTS]        
//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing
light.0=1, -68.50,   0.00,  28.60, fx_beaconh ,
light.1=1, -52.50,   0.00, 0.8, fx_beaconb ,
light.2 = 4, 45.00,    -1.00,    6.00, tu104_vclight ,
light.3 = 4, 45.00,    1.00,    6.00, tu104_vclight ,
light.4 = 4, 50.00,    -1.00,    4.00, tu104_vclight ,

[effects]
wake = fx_wake
water = fx_spray
dirt = fx_tchdrt
concrete = fx_sparks
touchdown = fx_tchdwn, 1
contrail=fx_A_I_Contrail

[smokesystem]
smoke.0 = 1.69, -39.30, -6.90, fx_smoke_rx
smoke.1 = 1.69, -39.30, 6.90, fx_smoke_rx

[forcefeedback]
gear_bump_nose_magnitude = 3000
gear_bump_nose_direction = 18000
gear_bump_nose_duration = 250000
gear_bump_left_magnitude = 2700
gear_bump_left_direction = 35500
gear_bump_left_duration = 250000
gear_bump_right_magnitude = 2700
gear_bump_right_direction = 00500
gear_bump_right_duration = 250000
ground_bumps_magnitude1 = 1300
ground_bumps_angle1 = 08900
ground_bumps_intercept1 = 3.0
ground_bumps_slope1 = 0.20
ground_bumps_magnitude2 = 200
ground_bumps_angle2 = 09100
ground_bumps_intercept2 = 1.075
ground_bumps_slope2 = 0.035
crash_magnitude1 = 10000
crash_direction1 = 01000
crash_magnitude2 = 10000
crash_direction2 = 9000
crash_period2 = 75000
crash_duration2 = 2500000

[direction_indicators]
direction_indicator.0=3,0

[brakes]
toe_brakes_scale=0.579852
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]
electric_pumps=0
engine_map=1,1,0,0
normal_pressure=3000.000000

[stall_warning]
type=1

[attitude_indicators]
attitude_indicator.0=1

[turn_indicators]
turn_indicator.0=1,0

[exits]
number_of_exits=2
exit_rate.0=1.0
exit_rate.1=1.0

[TailHook]
tailhook_length=4
tailhook_position = -15.0, 0.0, -1.0
cable_force_adjust = 1.0

[folding_wings]
wing_fold_system_type=4
fold_rates=30,30

[pitot_static]
vertical_speed_time_constant = 1