[fltsim.0] title=Polikarpov Po-2 28 sim=Po2rk model=1 panel= sound= texture=28 kb_checklists= kb_reference= atc_id=28 prop_anim_ratio=-1.42 ui_manufacturer=Polikarpov ui_type=Po-2LNB ui_variation=9th GbNBAD description=9th GbNBAD\nserial 28\nSeptember 1944\nMission of Polish insurgents supply [fltsim.1] title=Polikarpov Po-2 9 sim=Po2rk model=1 panel= sound= texture=9 kb_checklists= kb_reference= atc_id=9 prop_anim_ratio=-1.42 ui_manufacturer=Polikarpov ui_type=Po-2LNB ui_variation=Korea North description=Korean Peoples Army Air Force\nNight Bomber Regiment\nserial 9\nearly 1951\nCommander Pak Ten Sik [fltsim.2] title=Polikarpov Po-2 10 sim=Po2rk model=1 panel= sound= texture=10 kb_checklists= kb_reference= atc_id=10 prop_anim_ratio=-1.42 ui_manufacturer=Polikarpov ui_type=Po-2LNB ui_variation=Normandie-Niemen description=Normandie-Niemen\nserial 10\nMonastirchina, September 1943\nliaison aircraft ////=================================================================================================== [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 im Reference position: (1/4 chord, centerline, waterline) empty_weight_CG_position = 1.0, 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, Machine Gun" //Weight, Lat, Lon, Vert Position station_load.3 = "60.0, -2.075, -6.0, -2.8, Bomb" //Weight, Lat, Lon, Vert Position station_load.4 = "60.0, -2.075, -4.8, -2.8, Bomb" //Weight, Lat, Lon, Vert Position station_load.5 = "60.0, -2.075, 4.8, -2.8, Bomb" //Weight, Lat, Lon, Vert Position station_load.6 = "60.0, -2.075, 6.0, -2.8, Bomb" //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 = 0.0 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= 40.2 //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 = 0.0 //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