[fltsim.0]
title=Utka
sim=mig8
model=
panel=
sound=
texture=
kb_checklists=
kb_reference=
description=In August 1945, the MiG Aircraft Factory began testing the experimental plane "Utka" (Duck).Testing continued about one year,then the bureau MiG used this plane for business flights.Only one plane was made with several changes during testflights - rudders, nosewheel, wingtips. 
ui_manufacturer=MiG
ui_type=MiG-8
ui_variation=Utka (former)
atc_heavy=0
atc_id=
atc_airline=Mikoyan
atc_flight_number=
editable=1
prop_anim_ratio=1.32
atc_id_color=0000800000
visual_damage=0

[fltsim.1]
title=Utka_2
sim=mig8
model=2
panel=
sound=
texture=2
kb_checklists=
kb_reference=
description=In August 1945, the MiG Aircraft Factory began testing the experimental plane "Utka" (Duck).Testing continued about 9 months,then the bureau MiG used this plane for business flights.Only one plane was made with several changes during testflights - rudders, nosewheel, wingtips.
ui_manufacturer=MiG
ui_type=MiG-8
ui_variation=Utka (later)
atc_heavy=0
atc_id=
atc_airline=Mikoyan
atc_flight_number=
editable=1
prop_anim_ratio=1.32
atc_id_color=0000800000
visual_damage=0

[General]
performance=Maximum Speed\t240 km/h (calculate)\nMaximum Speed\t215 km/h (achieved)\nTakeOff/On Speed 103/92 km/h\nStall Speed 77 km/h\nMaximum Range\t500 km\nFuel Capacity\t118 l\nMax Gross Weight\t1150 kg\nEmpty Weight\t746 kg\nSeats\t3\nShvetsov M-11FM five cylinder air-cooled radial engine, 82 kW (110 hp)\n2-bladed pusher propeller, 2.36m diameter\n\n 
atc_type=MiG 
atc_model=Utka
editable=0 
Category=airplane

[weight_and_balance]
max_gross_weight =2536.3
empty_weight = 1646.6
reference_datum_position = 0, 0, 0
empty_weight_CG_position = 0, 0, 0
empty_weight_pitch_MOI = 7400
empty_weight_roll_MOI = 5137
empty_weight_yaw_MOI = 4360
empty_weight_coupled_MOI = 0
max_number_of_stations = 4

station_load.0 = "165, 4,  0,   -0.45, Pilot"
station_load.1 = "0,   0,  1.5, -1.0,  Passenger1"
station_load.2 = "0,  -3, -1.5, -1.0,  Passenger2"
station_load.3 = "30, -3, -2.5, -1.0,  Baggage"

[flight_tuning]
cruise_lift_scalar=1.000
pitch_stability=1.200
roll_stability=1.200
yaw_stability=1.200
parasite_drag_scalar=1.100
induced_drag_scalar=1.100
elevator_effectiveness=0.900            
aileron_effectiveness=0.9000
rudder_effectiveness=0.9000

[lights]
//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit
light.0 = 3, -5.5,  -15.5, 0.35,    fx_navred         // (feet) longitudinal, lateral, vertical 
light.1 = 3, -5.5,   15.5, 0.35,    fx_navgre
light.4 = 5,  12.0,  0,   -2.15,    fx_landing
light.6 = 4,  5,     0,    1,       fx_vclight

[GeneralEngineData]
engine_type = 0
fuel_flow_scalar = 1
engine.0 = -4.1, 0, 0.2,
min_throttle_limit=0.05

//[smokesystem]


[effects]


[fuel]
LeftMain=0,-2,0,15.58
RightMain=0,2,0,15.58
fuel_type=1
number_of_tank_selectors=1
electric_pump=1

//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]
//-------------------------------------------------------------------------------------------
//       0      1       2       3         4    5     6      7    8      9   10    11   12   13                      -1-         -3- 
//-------------------------------------------------------------------------------------------

point.0 = 1,   10,      0,    -5.5,     1500,  0,  0.45,  30.0, 0.07,  2.5, 0.7, 5, 3, 0, 120, 205
point.1 = 1,  -1,      -5.0,  -5.65,    1500,  1,  0.55,   0,   0.3,   2.5, 0.7, 5, 3, 2, 120, 205
point.2 = 1,  -1,       5.0,  -5.65,    1500,  2,  0.55,   0,   0.3,   2.5, 0.7, 5, 3, 3, 120, 205

point.3 = 2,   0,     -18,     2.1,     1575,  0,  0,      0,   0,     0,   0,   0, 0, 5, 0,   0
point.4 = 2,   0.0,    18,     2.1,     1575,  0,  0,      0,   0,     0,   0,   0, 0, 6, 0,   0
point.5 = 2,  -5.2,    0,     -1.7,     1575,  0,  0,      0,   0,     0,   0,   0, 0, 9, 0,   0
point.6 = 2,  12,      0,     -0.3,     1575,  0,  0,      0,   0,     0,   0,   0, 0, 4, 0,   0
point.7 = 2, -16.3,    0,      6.8,     1575,  0,  0,      0,   0,     0,   0,   0, 0, 7, 0,   0
point.8 = 2,  -1,      0,     -1.3,     1575,  0,  0,      0,   0,     0,   0,   0, 0, 8, 0,   0
point.9 = 2, -7.2,    13.2,    4.1,     1575,  0,  0,      0,   0,     0,   0,   0, 0, 7, 0,   0
point.10 =2, -7.2,   -13.2,    4.1,     1575,  0,  0,      0,   0,     0,   0,   0, 0, 8, 0,   0
point.11 =5,  0,       0,      0,          0,  0,  0,      0,   0,     0,   0,   2, 4, 0, 10, 30
point.12 =5,  0,       0,      0,          0,  0,  0,      0,   0,     0,   0,   4, 2, 0, 10, 30
point.13 =2, 7.7,      6.05,   0,          0,  0,  0,      0,   0,     0,   0,   0, 0, 7, 0, 0
point.14 =2, 7.7,     -6.05,   0,          0,  0,  0,      0,   0,     0,   0,   0, 0, 8, 0, 0
gear_system_type=0
static_pitch = 0
static_cg_height = 5.0
max_number_of_points = 15

[keyboard_response]
elevator = 100, 180
aileron = 200, 1000
rudder = 200, 1000

[forcefeedback]

[airplane_geometry]
wing_area = 162
wing_span = 31
wing_root_chord = 4.92
wing_dihedral = 1
wing_incidence = 0.02
wing_twist = -3
oswald_efficiency_factor = 0.56
wing_winglets_flag = 1
wing_sweep = 20
wing_pos_apex_lon = 1.3
wing_pos_apex_vert = 0
htail_area = 23
htail_span = 15.7
htail_pos_lon = -11             //8.92
htail_pos_vert = 0
htail_incidence = 3.25
htail_sweep = 0
vtail_area = 29                   //24
vtail_span = 5.58
vtail_sweep = 0
vtail_pos_lon = -5.2
vtail_pos_vert = 2.5
elevator_area = 16.6
aileron_area = 18.3
rudder_area = 6.65
elevator_up_limit = 25
elevator_down_limit = 25
aileron_up_limit = 20
aileron_down_limit = 15
rudder_limit = 24
elevator_trim_limit = 19.5
spoiler_limit = 573
aileron_to_spoileron_gain = 0
min_ailerons_for_spoilerons = 0
min_flaps_for_spoilerons = 0
spoilerons_available = 0
auto_spoiler_available=0
spoiler_extension_time=2.000000
positive_g_limit_flaps_up=4.000000
positive_g_limit_flaps_down=2.000000
negative_g_limit_flaps_up=-1.500000
negative_g_limit_flaps_down=-1.500000

[electrical]
max_battery_voltage = 24
generator_alternator_voltage = 28
max_generator_alternator_amps = 60

fuel_pump = 0, 5, 17
starter1 = 0, 20, 17
light_nav = 0, 5, 17

light_panel = 0, 5, 17

//[Flaps.0]
//type=1
//span-outboard=0.5
//extending-time=7
//system_type=0
//flaps-position.0=0,0
//flaps-position.1=38,0

[piston_engine]
cylinder_displacement=90.252 
compression_ratio=8.5 
number_of_cylinders=5 
max_rated_rpm=2400 
max_rated_hp=160                    //260 
fuel_metering_type=1 
cooling_type=0 
normalized_starter_torque=0.3 
turbocharged=0
max_design_mp=47 
min_design_mp=10 
critical_altitude=9800 
emergency_boost_type=0 
emergency_boost_mp_offset=0 
emergency_boost_gain_offset=0 
fuel_air_auto_mixture=1 
auto_ignition=0 
max_rpm_mechanical_efficiency_scalar=1 
idle_rpm_mechanical_efficiency_scalar=1 
max_rpm_friction_scalar=1 
idle_rpm_friction_scalar=1 

[propeller]
rotation=-1
propeller_type=0 
propeller_diameter=7.708
propeller_blades=2 
propeller_moi=5.7 
beta_max=32 
beta_min=17 
min_gov_rpm=1400 
prop_tc=0.1 
gear_reduction_ratio=1 
fixed_pitch_beta=20 
low_speed_theory_limit=80 
prop_sync_available=0 
prop_deice_available=0 
prop_feathering_available=0 
prop_auto_feathering_available=0 
min_rpm_for_feather=0 
beta_feather=0 
power_absorbed_cf=0 
defeathering_accumulators_available=0 
prop_reverse_available=0 
minimum_on_ground_beta=0 
minimum_reverse_beta=0 

[Reference Speeds]
flaps_up_stall_speed=45 
full_flaps_stall_speed=45 
cruise_speed=100 
max_indicated_speed=130

[pitot_static]
vertical_speed_time_constant = 1.5
pitot_heat=1.000000

[exits]
number_of_exits = 1
exit_rate.0 = 1.0
//exit_rate.1 = 0.2

[views]
eyepoint= 3.05, 0, 0.5

[direction_indicators]
direction_indicator.0=1, 0 

[autopilot]
autopilot_available=0
flight_director_available=0 
default_vertical_speed=0.001 
autothrottle_available=0 
pitch_takeoff_ga=8 
max_pitch=10
max_pitch_acceleration=1
max_pitch_velocity_lo_alt=2
max_pitch_velocity_hi_alt=1.5
max_pitch_velocity_lo_alt_breakpoint=20000
max_pitch_velocity_hi_alt_breakpoint=28000
max_bank=25
max_bank_acceleration=1.8
max_bank_velocity=3
max_throttle_rate=0.1
nav_proportional_control=9
nav_integrator_control=0.25
nav_derivative_control=0
nav_integrator_boundary=2.5
nav_derivative_boundary=0
gs_proportional_control=9.52
gs_integrator_control=0.26
gs_derivative_control=0
gs_integrator_boundary=0.7
gs_derivative_boundary=0
yaw_damper_gain=0
autothrottle_arming_required=0
autothrottle_takeoff_ga=0
autothrottle_max_rpm=90.000000

[Radios]
// Radio Type = availiable, standby frequency, has glide slope
Audio.1       = 1
Com.1         = 1
Com.2         = 1
Transponder.1 = 1
Marker.1      = 1

[brakes]
toe_brakes_scale=0.8
parking_brake=1
differential_braking_scale=1.0

[gear_warning_system]
gear_warning_available=1
pct_throttle_limit=0.3


[hydraulic_system]
normal_pressure=0

[stall_warning]
type=2
stick_shaker=1

[attitude_indicators]
attitude_indicator.0=1

[turn_indicators]
turn_indicator.0=1,0

//[Flaps.0]
//type=1
//span-outboard=0.500000
//extending-time=3.000000
//system_type=0
//flaps-position.0=0.000000,0.000000
//flaps-position.1=37.998561,0.000000
[Flaps.0]
type=1
span-outboard=0.500000
extending-time=3.000000
system_type=0
[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=0.000000
[deice_system]
structural_deice_type=0