[fltsim.0]
title=Antonov An8
sim=An8
model=
panel=
sound=
texture=
kb_checklists=An8_Check
kb_reference=
ui_manufacturer=Antonov
ui_type=An8 
ui_variation=Aeroflot
atc_id=2721
prop_anim_ratio=-1.53
atc_airline=Aeroflot 
atc_flight_number=2721
description=Antonov An-8 Выпуск 1956г. (Летающий кит) Модифицировался в разных вариантах.В некоторых странах до сих пор эксплуатируется.Потолок 9600.  Максимальная скорость 500-520км\ч. Крейсерская скорость 450-470км\ч. Экипаж 6 человек.

\\\=======================================

[General]
performance=An8
atc_type=An8
atc_model=An8
editable=0


\\\=====================================================================================================
///====================================================
///====================================================
///====================================================

[WEIGHT_AND_BALANCE]
;Place for comments

empty_weight = 29800

reference_datum_position     =    0.0, 0, 0
empty_weight_CG_position     =  -1.79, 0, 0

empty_weight_roll_MOI=2363372.000000
empty_weight_pitch_MOI=3172439.000000
empty_weight_yaw_MOI=2588164.000000
empty_weight_coupled_MOI=0.000000
max_number_of_stations=50
station_load.0=0.000000,0.000000,0.000000,0.000000
max_gross_weight=45000.000000

///====================================================
///====================================================
///====================================================

[flight_tuning]
cruise_lift_scalar=1.000
parasite_drag_scalar=0.900
induced_drag_scalar=0.900
elevator_effectiveness=1.000
aileron_effectiveness=1.000
rudder_effectiveness=0.950
pitch_stability=1.000
roll_stability=1.000
yaw_stability=1.100
elevator_trim_effectiveness=0.810
aileron_trim_effectiveness=1.000
rudder_trim_effectiveness=1.000

///====================================================
///====================================================
///====================================================

[GeneralEngineData]
engine_type=5
Engine.0=7.620,-14.190,1.80
Engine.1=7.620,14.190,1.80
fuel_flow_scalar=0.75
min_throttle_limit=-0.20

[TurbineEngineData]
fuel_flow_gain=0.005
inlet_area=1.100
rated_N2_rpm=29920.000
static_thrust=400.000  \\\400
afterburner_available=0

[turboprop_engine]
power_scalar=1.05
maximum_torque=11124.000
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= 1.21      \\\1.25
propeller_type=0
propeller_diameter=17.400
propeller_blades=4
propeller_moi=80.000
beta_max=45.0
beta_min=11.500
min_gov_rpm=24994.000
prop_tc=0.002
gear_reduction_ratio=24.686400
fixed_pitch_beta=0.000
low_speed_theory_limit=80.000
prop_sync_available=1
prop_deice_available=1
prop_feathering_available=1
prop_auto_feathering_available=1
min_rpm_for_feather=350.000
beta_feather=79.300
power_absorbed_cf=0.900
defeathering_accumulators_available=0
prop_reverse_available=1
minimum_on_ground_beta=0.000
minimum_reverse_beta=-20.000

[fuel]
// Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)
Center1=0.00,  0.00, 0.00,300.0, 400.0
LeftMain=0.00,-8.5, -1.00,  500.0, 400.0
RightMain=0.00, 8.5, -1.00,  500.0, 400.0
LeftAux=    -0.45, -20.0,  -2.33,   100.00
RightAux=   -0.45,  20.0,  -2.33,   100.00
number_of_tank_selectors=1
electric_pump=0
fuel_type=2.000000

///==========================================================================
///====================================================
///====================================================


[contact_points]
static_pitch = 0.8
static_cg_height = 10
tailwheel_lock = 0
gear_system_type = 1
max_number_of_points = 9


point.0 = 1.000, 34.480, 0.000, -10.5694, 1810.000, 0.000, 1.480, 35.000, 0.260, 2.500, 0.426, 4.000, 6.000, 0.000, 0.000, 300.000
point.1 = 1,   -6.0,  -10.8,  -10.05, 2300,  1,   2.47,  0.0,   0.40, 2.5, 0.80, 8.9, 8.7, 2, 0, 0
point.2 = 1,   -5.9,   10.8,  -10.05, 2300,  2,   2.47,  0.0,   0.40, 2.5, 0.80, 8.6, 8.3, 3, 0, 0
point.3 = 0,  -0.33, -50.0,   -2.91,  1700,  0.00,0.00,0.00,0.00,0.00,0.00,0.00,0.00,5.00,0.00,0.00
point.4 = 2,  -0.33,  50.0,   -2.91,  1700,  0.00,0.00,0.00,0.00,0.00,0.00,0.00,0.00,6.00,0.00,0.000
point.5 = 2,  -74.7,   0,      10.62,  1700.  0, 0, 0, 0, 0, 0, 0, 0, 0, 9, 0, 0
point.6 = 2,   49.7,   0,       0.12,   1700.  0, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0
point.7 = 2, 3.9635, -8.1788, -6.4699, 0, 0, 0, 0, 0, 0, 0, 0, 0, 7, 0, 0
point.8 = 2, 3.9635, 8.1788, -6.4699, 0, 0, 0, 0, 0, 0, 0, 0, 0, 8, 0, 0


///=======================================
///====================================================
///====================================================

[flaps.0]
type             = 1                                    // 1 - tail, 2 - lead
span-outboard    = 0.8                                  // 0.0 .. 1.0
extending-time   = 25                                   // seconds
flaps-position.0 = 0                                    // degrees
flaps-position.1 = 1                                    // degrees
flaps-position.2 = 5                                    // degrees
flaps-position.3 = 10                                   // degrees
flaps-position.4 = 20                                   // degrees
flaps-position.5 = 25                                   // degrees
flaps-position.6 = 30                                   // degrees
damaging-speed   = 200                                  // KIAS
blowout-speed    = 250                                  // KIAS
lift_scalar = 0.7
drag_scalar = 0.9
pitch_scalar= 0.9
system_type = 1                                         //Hydraulic

[flaps.1]
type             = 2                                    // 1 - tail, 2 - lead
span-outboard    = 0.8                                  // 0.0 .. 1.0
extending-time   = 2                                    // seconds
flaps-position.0 = 0                                    // degrees
flaps-position.1 = 1.0                                  // degrees
damaging-speed   = 250                                  // KIAS
blowout-speed    = 300                                  // KIAS
lift_scalar = 0.3
drag_scalar = 0.1
pitch_scalar= 0.1
system_type = 1                                         //Hydraulic


///=========================================
///====================================================
///====================================================

[Views]
eyepoint=0.19, -1.77, 1.71 


///eyepoint=18.7, -1.77, 1.74    //(feet) longitudinal, lateral, vertical distance from reference datum

///=========================================
///====================================================
///====================================================

[exits]
number_of_exits = 2
exit_rate.0 = 0.053                             ;Percent per second
exit_rate.1 = 0.2                               ;Percent per second

[TailHook]
tailhook_length=4                               ;(feet)
tailhook_position = -15.0, 0.0, -1.0            ;(feet) longitudinal, lateral, vertical positions from datum
cable_force_adjust = 1.0

[folding_wings]
wing_fold_system_type=4                       ;0=None
fold_rates=0.075,0.075	                          ;Percent per second

///====================================================
///====================================================

[lights]

//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing

light.0 = 3, 5.44, -60.16, 3.63, fx_navredm
light.1 = 3, 5.44, 60.16, 3.63, fx_navgrem
light.2 = 3, -47.70, 0, 9.71, fx_navwhih
light.3 = 1, -39.97, 0, 24.75, fx_beaconb
light.4 = 1, -3.14, 0, -6.52, fx_beaconb



[effects]
wake = fx_wake
water = fx_spray
dirt = fx_tchdrt
concrete = fx_sparks
touchdown = fx_td, 1
windshield_rain_effect_available = 1

///====================================================
[autopilot]
autopilot_available=1
flight_director_available=1
default_vertical_speed=500
use_no_default_pitch=0		// 0 = Default to current pitch mode, 1 = No default pitch mode.
use_no_default_bank=0		// 0 = Default to Wing Leveler mode, 1 = No default bank mode.
autothrottle_available=1
autothrottle_arming_required=-256
autothrottle_takeoff_ga=-256
autothrottle_max_rpm=90.000
pitch_takeoff_ga=8.000
autoland_available=1
max_pitch=10.000000
max_pitch_acceleration=1.000000
max_pitch_velocity_lo_alt=2.000000
max_pitch_velocity_hi_alt=1.500000
max_pitch_velocity_lo_alt_breakpoint=20000.000000
max_pitch_velocity_hi_alt_breakpoint=28000.000000
max_bank=25.000000
max_bank_acceleration=1.800000
max_bank_velocity=3.000000
max_throttle_rate=0.100000
nav_proportional_control=9.000000
nav_integrator_control=0.250000
nav_derivative_control=0.000000
nav_integrator_boundary=2.500000
nav_derivative_boundary=0.000000
gs_proportional_control=9.520000
gs_integrator_control=0.260000
gs_derivative_control=0.000000
gs_integrator_boundary=0.700000
gs_derivative_boundary=0.000000
yaw_damper_gain=0.000000

///====================================================
[Radios]
// Radio Type = availiable, standby frequency, has glide slope
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 = 0
Marker.1      = 1

///====================================================
[brakes]
toe_brakes_scale=1.33
parking_brake=1

///====================================================

[airplane_geometry]
wing_area=753.000
wing_span=95.120
wing_root_chord=11.200
wing_dihedral=2.500
wing_incidence=2.500
wing_twist=-0.967
oswald_efficiency_factor=0.750
wing_winglets_flag=0
wing_sweep=6.000
wing_pos_apex_lon=1.000
wing_pos_apex_vert=5.100
htail_area=149.000
htail_span=32.520
htail_pos_lon=-37.600
htail_pos_vert=4.100
htail_incidence=0.000
htail_sweep=10.000
vtail_area=186.000
vtail_span=14.103
vtail_sweep=25.000
vtail_pos_lon=-33.030
vtail_pos_vert=5.100
elevator_area=35.600
aileron_area=59.400
rudder_area=56.000
elevator_up_limit=30.000
elevator_down_limit=20.000
aileron_up_limit=25.000
aileron_down_limit=25.000
rudder_limit=30.00
elevator_trim_limit=22.480565
spoiler_limit=90.000
spoilerons_available=0
aileron_to_spoileron_gain=0.000
min_ailerons_for_spoilerons=0.000
min_flaps_for_spoilerons=0.000

///===========================================MISK===============
///==============================================================
///==============================================================

[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

[Reference Speeds]
flaps_up_stall_speed=98.000000
full_flaps_stall_speed=78.000000
cruise_speed=240.000
max_indicated_speed=324.000000
max_mach=0.656982

[pitot_static]
vertical_speed_time_constant=2.0	// Increasing this value will cause a faster reaction in the VSI

[gear_warning_system]
gear_warning_available=1
pct_throttle_limit=0.099976
flap_limit_power=25.783101
flap_limit_idle=15.011494
[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

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

[forcefeedback]
stick_shaker_magnitude=8000		; 0 - 10000
stick_shaker_direction=18000		; 0 - 35999 degrees
stick_shaker_period=111111		; in microseconds
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=5700		; 0 - 10000
gear_bump_left_direction=355000		; 0 - 35999 degrees
gear_bump_left_duration=250000		; in microseconds
gear_bump_right_magnitude=5700		; 0 - 10000
gear_bump_right_direction=79000		; 0 - 35999 degrees
gear_bump_right_duration=250000		; in microseconds
ground_bumps_magnitude1=3300		; 0 - 10000
ground_bumps_angle1=08900		; 0 - 35999 degrees
ground_bumps_intercept1=5.0
ground_bumps_slope1=0.48
ground_bumps_magnitude2=720		; 0 - 10000
ground_bumps_angle2=09100		; 0 - 35999 degrees
ground_bumps_intercept2=0.075
ground_bumps_slope2=1.035
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 microseconds
///====================================================END!!!==============================