[fltsim.0]
title=Polikarpov Po-2 THK
sim=Po2rk
model=2
panel=2
sound=
texture=THK
kb_checklists=
kb_reference=
atc_id=04
prop_anim_ratio=-1.42
ui_manufacturer=Polikarpov
ui_type=Po-2
ui_variation=THK
description=THK (Turkish Air league) was founded in 1925. Its first name was TTC (Turk Tayyare Cemiyeti = Turkish Airplane Society). The first plane they bought was Polikarpov U-2. Two of them remained in service until 1945. The plane was very much loved by the Turkish civilian aviators due to its stability and performance.
[fltsim.1]
title=Polikarpov Po-2 RK
sim=Po2rk
model=2
panel=
sound=
texture=test
kb_checklists=
kb_reference=
atc_id=02
prop_anim_ratio=-1.42
ui_manufacturer=Polikarpov
ui_type=Po-2
ui_variation=RK
description=Polikarpov Po-2\n fictional repaint for testing
[fltsim.2]
title=Polikarpov Po-2 DM-WCR
sim=Po2rk
model=2
panel=
sound=
texture=DM-WCR
kb_checklists=
kb_reference=
atc_id=DM-WCR
prop_anim_ratio=-1.42
ui_manufacturer=Polikarpov
ui_type=Po-2
ui_variation=Aeroclub Technical University Dresden
description=Aeroclub Technical University/nDresden, 1959
[fltsim.3]
title=Polikarpov Po-2 DM-WAL
sim=Po2rk
model=3
panel=
sound=
texture=DM-WAL
kb_checklists=
kb_reference=
atc_id=DM-WAL
prop_anim_ratio=-1.42
ui_manufacturer=Polikarpov
ui_type=Po-2
ui_variation=GST 1959 DM-WAL
description=GST, Circa 1959 \nDSF is German-Soviet Friendship association
[fltsim.4]
title=Polikarpov Po-2 DM-WAB
sim=Po2rk
model=4
panel=
sound=
texture=DM-WAB
kb_checklists=
kb_reference=
atc_id=DM-WAB
prop_anim_ratio=-1.42
ui_manufacturer=Polikarpov
ui_type=Po-2
ui_variation=GST 1957 DM-WAB
description=GST, Circa 1957
[General]
atc_type=Polikarpov
atc_model=PO2
editable=0
////===================================================================================================
////===================================================================================================
performance=\n
[WEIGHT_AND_BALANCE]
max_gross_weight = 2980 // (pounds)
empty_weight = 1700 // (pounds)
reference_datum_position = 0, 0, 0 // (feet) distance from F
empty_weight_CG_position = 0.5, 0, 0 // (feet) longitudinal, lateral, vertical distance from specified datum
max_number_of_stations =50
station_load.0 = "170.0, -2.393, 0.0, -2.0, Pilot" //Weight, Lat, Lon, Vert Position
station_load.1 = "170.0, -4.817, 0.0, -2.0, Co-Pilot" //Weight, Lat, Lon, Vert Position
station_load.2 = "100.0, -7.396, 0.0, 3.5, Bagage" //Weight, Lat, Lon, Vert Position
;Moments of Inertia
empty_weight_pitch_MOI = 2585
empty_weight_roll_MOI = 606
empty_weight_yaw_MOI = 12023
empty_weight_coupled_MOI = 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 = 1.0
aileron_trim_effectiveness = 0.0
rudder_trim_effectiveness = 0.0
p_factor_on_yaw = 0.5
torque_on_roll = 1.0
gyro_precession_on_yaw = 1.0
gyro_precession_on_pitch = 1.0
////===================================================================================================
[GeneralEngineData]
engine_type = 0 //0=Piston, 1=Jet, 2=None, 3=Helo-Turbine, 4=Rocket, 5=Turboprop
Engine.0 = 5.064, 0.0, 0.0 //(feet) longitudinal, lateral, vertical distance from reference datum
fuel_flow_scalar= 1.0 //Fuel flow scalar
min_throttle_limit = 0.0 //Minimum percent throttle. Generally negative for turbine reverser
master_ignition_switch = 1 //Master Ignition Switch
////===================================================================================================
[piston_engine]
power_scalar = 1.0 //Piston power scalar
cylinder_displacement= 105 //Cubic inches per cylinder
compression_ratio= 5.0 //Compression ratio
number_of_cylinders= 5 //Number of cylinders
max_rated_rpm= 2200 //Max rated RPM
max_rated_hp= 150 //Max rated HP
fuel_metering_type= 1 //0=Fuel Injected, 1=Gravity Carburetor, 2=Aerobatic Carburetor
cooling_type= 0 //0=Cooling type Air, 1=Cooling type Liquid
normalized_starter_torque= 0.3 //Starter torque factor
turbocharged= 0 //Is it turbocharged? 0=FALSE, 1=TRUE
max_design_mp= 47 //Max design manifold pressure, (inHg)
min_design_mp= 10 //Min design manifold pressure, (inHg)
critical_altitude= 9800 //Altitude to which the turbocharger will provide max design manifold pressure (feet)
emergency_boost_type= 0 //0=None, 1=Water Injection, 2=Methanol/Water injection, 3=War Emergency Power
emergency_boost_mp_offset= 0 //Additional manifold pressure supplied by emergency boost
emergency_boost_gain_offset= 0 //Multiplier on manifold pressure due to emergency boost
fuel_air_auto_mixture= 1 //Automixture available? 0=FALSE, 1=TRUE
auto_ignition= 1 //Auto-Ignition available? 0=FALSE, 1=TRUE
max_rpm_mechanical_efficiency_scalar= 1.0 //Scalar on maximum RPM mechanical efficiency
idle_rpm_mechanical_efficiency_scalar= 1.0 //Scalar on idle RPM mechanical efficiency
max_rpm_friction_scalar= 1.0 //Scalar on maximum RPM friction
idle_rpm_friction_scalar= 1.0 //Scalar on idle RPM friction
////===================================================================================================
[propeller]
thrust_scalar = 0.9 //Propeller thrust scalar
propeller_type= 0 //0=Constant Speed, 1=Fixed Pitch
propeller_diameter= 8.093 //Propeller Diameter, (feet)
propeller_blades= 2 //Number of propeller blades
propeller_moi= 9.93 //Propeller moment of inertia
beta_max= 30.0 //Maximum blade pitch angle for constant speed prop, (degrees)
beta_min= 18.0 //Minimum blade pitch angle for constant speed prop, (degrees)
min_gov_rpm= 1400 //Miminum governed RPM
prop_tc= 0.1 //Prop time-constant
gear_reduction_ratio= 1.0 //Propeller gear reduction ratio
fixed_pitch_beta= 0.0 //Fixed pitch angle of fixed pitch prop, (degrees)
low_speed_theory_limit= 80.0 //Speed at which low speed theory becomes blended in (feet/second)
prop_sync_available= 1 //Prop synchronization available? 0=FALSE, 1=TRUE
prop_deice_available= 1 //Prop de-icing available? 0=FALSE, 1=TRUE
prop_feathering_available= 1 //Prop feathering available? 0=FALSE, 1=TRUE
prop_auto_feathering_available= 0 //Prop auto-feathering available? 0=FALSE, 1=TRUE
min_rpm_for_feather= 700.0 //Minimum RPM for prop feathering
beta_feather= 89.5 //Feathering pitch angle (degrees)
power_absorbed_cf= 0.9 //Coefficient of friction for power absorbed by propeller in feather
defeathering_accumulators_available= 0 //Defeathering accumulators available? 0=FALSE, 1=TRUE
prop_reverse_available= 0 //Prop reverse available? 0=FALSE, 1=TRUE
minimum_on_ground_beta= 0.0 //Miminum pitch angle on ground, (degrees)
minimum_reverse_beta= 0.0 //Minimum pitch angle in reverse, (degrees)
feathering_switches = 1 //Switches which invoke feathering
////===================================================================================================
///================================================================================
[Views]
eyepoint = -2.353, -0.0, 2.236 //Pilot
//eyepoint = -4.641, -0.0, 2.236 //Backseater
///================================================================================
[fuel]
Center1 = 0.5, 0.0, -0.7, 100.0, 0.0 //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)
fuel_type = 1 //Fuel type: 1 = Avgas, 2 = JetA
number_of_tank_selectors =1
electric_pump= 0
////===================================================================================================
[smokesystem]
smoke.0 = -2.18, 0, 3, fx_smoke_rx
smoke.1 = -2.18, 0, -3, fx_smoke_rx
////===================================================================================================
[EFFECTS]
wake=fx_wake
water=fx_spray
dirt=fx_tchdrt
concrete=fx_sparks
startup=fx_engstrt_jenny
touchdown=fx_tchdwn_s, 1
////===================================================================================================
[contact_points]
//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
max_number_of_points = 9
// Cl LON LAT VERT IDT BM RAD STE SCOM CRA DR ET RT S
point.0 = 1, -18.28, 0.0, -2.53, 1500, 0, 0.5, 0, 0.0, 1.0, 2.00, 0, 0, 0
point.1 = 1, -0.55, -2.76, -6.13, 3200, 1, 0.9, 0, 0.5, 1.2, 0.28, 0, 0, 2
point.2 = 1, -0.55, 2.76, -6.13, 3200, 2, 0.9, 0, 0.5, 1.2, 0.29, 0, 0, 3
//point.0 = 1, -9.447, 0.0000, -3.412, 1500, 0, 0.5, 45, 0.5, 2.5, 0.30, 0, 0, 0, 0, 0
//point.1 = 1, 7.882, -5.0798, -5.242, 3500, 1, 0.9, 0, 0.8, 1.0, 0.99, 5, 5, 2, 0, 0
//point.2 = 1, 7.882, 5.0798, -5.242, 3500, 2, 0.9, 0, 0.8, 1.0, 0.99, 5, 5, 3, 0, 0
point.3= 2, -3.41, -13.92, -2.93, 1200, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0
point.4= 2, -3.41, 13.92, -2.93, 1200, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0
static_pitch = 12
static_cg_height = 5.6
tailwheel_lock = 1
//static_pitch = 12.0
//static_cg_height = 4.6
//gear_system_type=4
//tailwheel_lock = 0
////===================================================================================================
[keyboard_response]
elevator = 100.000000, 180.000000
aileron = 200.000000, 1000.000000
rudder = 200.000000, 1000.000000
[forcefeedback]
gear_bump_nose_magnitude = 6000
gear_bump_nose_direction = 18000
gear_bump_nose_duration = 250000
gear_bump_left_magnitude = 6000
gear_bump_left_direction = 35500
gear_bump_left_duration = 250000
gear_bump_right_magnitude = 6000
gear_bump_right_direction = 00500
gear_bump_right_duration = 250000
ground_bumps_magnitude1 = 3250
ground_bumps_angle1 = 8900
ground_bumps_intercept1 = 5.0
ground_bumps_slope1 = 0.48
ground_bumps_magnitude2 = 750
ground_bumps_angle2 = 9100
ground_bumps_intercept2 = 0.075
ground_bumps_slope2 = 1.0
crash_magnitude1 = 10000
crash_direction1 = 01000
crash_magnitude2 = 10000
crash_direction2 = 9000
crash_period2 = 75000
crash_duration2 = 2500000
////===================================================================================================
[airplane_geometry]
wing_area = 357.0 //Square feet
wing_span = 37.5 //Feet
wing_root_chord = 5.85 //Feet
wing_dihedral = 3.0 //Degrees
wing_incidence = 0.0 //Degrees
wing_twist = -1.0 //Degrees
oswald_efficiency_factor= 0.95 //Measure of lift effeciency of wing
wing_winglets_flag = 0 //Are winglets available?
wing_sweep = 0.0 //Degrees, wing leading edge
wing_pos_apex_lon = 1.58 //Feet, longitudinal distance from reference point, negative going aft
wing_pos_apex_vert = -2.7 //Feet, vertical distance from reference point, positive going up
htail_area = 95.8 //Square feet
htail_span = 15.25 //Feet
htail_pos_lon = -16.7 //Feet, longitudinal distance from reference point, negative going aft
htail_pos_vert = 1.0 //Feet, vertical distance from reference point, positive going up
htail_incidence = 0.0 //Degrees
htail_sweep = 0.0 //Degrees, horizontal tail leading edge
vtail_area = 67.9 //Square feet
vtail_span = 6.49 //Feet, tip to body
vtail_sweep = 50.4 //Degrees, vertical tail leading edge
vtail_pos_lon = -16.7 //Feet, longitudinal distance from reference point, negative going aft
vtail_pos_vert = 0.0 //Feet, vertical distance from reference point, positive going up
elevator_area = 53.4 //Square feet
aileron_area = 102.8 //Square feet
rudder_area = 65.7 //Square feet
elevator_up_limit = 20.0 //Degrees
elevator_down_limit = 20.0 //Degrees
aileron_up_limit = 27.0 //Degrees
aileron_down_limit = 18.0 //Degrees
rudder_limit = 30.0 //Degrees
elevator_trim_limit = 20 //Degrees
spoiler_limit = 0.0 //Degrees
spoilerons_available = 0 //Spoilerons Available?
aileron_to_spoileron_gain = 0 //Aileron to spoileron gain
min_ailerons_for_spoilerons = 0 //Degrees
min_flaps_for_spoilerons = 0 //Minimum flap handle position when spoilerons activate
////===================================================================================================
[electrical]
max_battery_voltage = 24
generator_alternator_voltage = 25
max_generator_alternator_amps = 10
////===================================================================================================
[Reference Speeds]
flaps_up_stall_speed = 35.5 //Knots True (KTAS)
cruise_speed = 59.0 //Knots True (KTAS)
max_indicated_speed = 82 //Red line (KIAS)
full_flaps_stall_speed=28.400000
////===================================================================================================
[autopilot]
autopilot_available=0
flight_director_available=0
////===================================================================================================
[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
direction_indicator.1=2,0
////===================================================================================================
[attitude_indicators]
//Type: 0=None, 1=Vacuum Gyro, 2=Electric Gyro
attitude_indicator.0 = 1
attitude_indicator.1 = 1
////===================================================================================================
[turn_indicators]
//Type: 0=None, 1=Electric Gyro, 2=Vacuum Gyro
turn_indicator.0=2,0
////===================================================================================================
[brakes]
parking_brake = 0 //Parking brake available
toe_brakes_scale = 0.85 //Brake scalar
differential_braking_scale = 1.0 //Delta on the amount of brake when the rudder pedals deflected
////===================================================================================================
[gear_warning_system]
gear_warning_available=0
pct_throttle_limit=0.000000
flap_limit_power=0.000000
flap_limit_idle=0.000000
////===================================================================================================
[hydraulic_system]
normal_pressure = 0.0 //PSI
electric_pumps = 0 //no electric pumps
engine_map = 1,0,0,0 //pump on Eng1
////===================================================================================================
[Radios]
// Radio Type = availiable, standby frequency, has glide slope
Audio.1 = 1
Com.1 = 1, 0
Com.2 = 1, 0
Nav.1 = 0, 0, 1
Nav.2 = 0, 0, 0
Adf.1 = 0
Adf.2 = 0
Transponder.1 = 0
Marker.1 = 1
////===================================================================================================
[stall_warning]
type=1
////===================================================================================================
[lights]
light.0 = 4, -1.14, 0.88, 1.02, fx_vclight,
[Flaps.0]
type=1
span-outboard=0.500000
extending-time=5.000000
system_type=1
flaps-position.0=0.000000,0.000000
flaps-position.1=8.571429,0.000000
flaps-position.2=17.142858,0.000000
flaps-position.3=25.714287,0.000000
flaps-position.4=34.285716,0.000000
flaps-position.5=42.857145,0.000000
flaps-position.6=51.428574,0.000000
flaps-position.7=60.000003,0.000000
