[fltsim.0] title=Yakovlev Yak 9 P sim=vercse model= panel= sound= texture= KB_checklists= kb_reference= atc_airline=HunAF atc_flight_number=17 ui_manufacturer=Yakovlev ui_type=Yak9p ui_variation=Vercse description=Vakovlev Yak9P HuAF 1950 [General] performance=Vércse - Windhover Fighter Category=airplane [weight_and_balance] max_gross_weight = 13514 empty_weight = 8260 reference_datum_position = 0, 0, 0 empty_weight_CG_position = 0, 0, 0 empty_weight_pitch_MOI = 48000 empty_weight_roll_MOI = 80000 empty_weight_yaw_MOI = 24000 empty_weight_coupled_MOI = 4000 max_number_of_stations = 2 station_load.0 = 210, -8, 0, 1.5 station_load.1 = 710, -10, 0, 1.5 [contact_points] static_pitch = 12 static_cg_height = 6.0 tailwheel_lock = 1 max_number_of_points = 10 point.0 = 1, -19, 0, -2.5, 9000.0, 0, 0.6, 36, 0.2, 2.5, 0.9, 8, 8.2, 0, 220.0, 250.0 point.1 = 1, 1.0, -5.0, -5.7, 9000.0, 1, 0.8, 0, 0.2, 2.5, 0.9, 9, 9.2, 2, 220.0, 250.0 point.2 = 1, 1.0, 5.0, -5.7, 9000.0, 2, 0.8, 0, 0.2, 2.5, 0.9, 8.5, 8.7, 3, 220.0, 250.0 point.3 = 2, 0.0, -20.00, -1.5, 8087, 0, 0, 0, 0, 0, 0, 0, 0, 5, 0, 0 point.4 = 2, 0.0, 20.00, -1.5, 8087, 0, 0, 0, 0, 0, 0, 0, 0, 6, 0, 0 point.5 = 2, -20.833, 0, -0.5, 8087, 0, 0, 0, 0, 0, 0, 0, 0, 9, 0, 0 point.6 = 2, 7.333, 0, -1.5, 8087, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0 point.7 = 2, -21, 0, 8.5, 8587, 0, 0, 0, 0, 0, 0, 0, 0, 7, 0, 0 point.8 = 2, 7, 0, 1.5, 8587, 0, 0, 0, 0, 0, 0, 0, 0, 8, 0, 0 point.9 = 2, 0, 0, 0, 8574, 0, 0, 0, 0, 0, 0, 0, 0, 5, 0, 0 gear_system_type=0 [GeneralEngineData] engine_type=0 Engine.0=3.7, 0, 0 Engine.1=3.7, 0, 0 fuel_flow_scalar=1 min_throttle_limit=0.0 [piston_engine] power_scalar=1 cylinder_displacement=181.722 compression_ratio=7.2 number_of_cylinders=18 max_rated_rpm=2700 max_rated_hp=2520 fuel_metering_type=0 cooling_type=0 normalized_starter_torque=0.033 turbocharged=1 max_design_mp=49.26 min_design_mp=9 critical_altitude=17500 emergency_boost_type=0 emergency_boost_mp_offset=0 emergency_boost_gain_offset=0 fuel_air_auto_mixture=0 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 fuel_flow_scalar = 1 emergency_boost_duration=360 [propeller] thrust_scalar=1 propeller_type=0 propeller_diameter=12 propeller_blades=3 propeller_moi=56.4 beta_max=65 beta_min=15 min_gov_rpm=405 prop_tc=0.1 gear_reduction_ratio=2.273 fixed_pitch_beta=30 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=700 beta_feather=88.5 power_absorbed_cf=0.9 defeathering_accumulators_available=0 prop_reverse_available=0 minimum_on_ground_beta=1 minimum_reverse_beta=-14 rotation=-1,-1 [keyboard_response] elevator = 200, 1000 aileron = 200, 1000 rudder = 200, 1000 [fuel] Center1=0, 0, -0.1, 97, 0 Center2=0, 0, -1, 30, 0 Center3=0, 0, 0, 17, 0 LeftMain=0, -9.4, -1.5, 28, 0 RightMain=0, 9.4, -1.5, 28, 0 // External1=0, -9, -1.4, 50, 0 // External2=0, 9, -1.4, 50, 0 fuel_type=1 number_of_tank_selectors=1 electric_pump=1 [forcefeedback] gear_bump_nose_magnitude = 3000 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 = 1500 ground_bumps_angle1 = 8900 ground_bumps_intercept1 = 5.0 ground_bumps_slope1 = 0.48 ground_bumps_magnitude2 = 750 ground_bumps_angle2 = 9100 crash_magnitude1 = 10000 crash_direction1 = 01000 crash_magnitude2 = 10000 crash_direction2 = 9000 crash_period2 = 75000 crash_duration2 = 2500000 stick_shaker_magnitude = 5000 stick_shaker_direction = 5000 stick_shaker_period = 111111 [airplane_geometry] wing_area = 222 wing_span = 34.3 wing_root_chord = 8.5 wing_dihedral = -2 wing_incidence = 1.000 wing_twist = 0.000000 oswald_efficiency_factor = 0.801 wing_winglets_flag = 0 wing_sweep = 35 wing_pos_apex_lon = 6.000 wing_pos_apex_vert = 0 htail_area = 49 htail_span = 11.33 htail_pos_lon = -15 htail_pos_vert = 5.75 htail_incidence = -0.989 htail_sweep = 35 vtail_area = 50 vtail_span = 6.7 vtail_sweep = 55 vtail_pos_lon = -8 vtail_pos_vert = 2 elevator_area = 56.390 aileron_area = 19.940 rudder_area = 15.040 elevator_up_limit = 16 elevator_down_limit = 32 aileron_up_limit = 15 aileron_down_limit = 15 rudder_limit = 30.000 elevator_trim_limit = 8 spoiler_limit = 0.0 aileron_to_spoileron_gain = 4.600 min_ailerons_for_spoilerons = 5 min_flaps_for_spoilerons = 0.000 spoilerons_available = 0 spoiler_handle_available=0 [electrical] max_battery_voltage = 24 generator_alternator_voltage = 28 max_generator_alternator_amps = 50 electric_always_available = 0 flap_motor = 0, 5, 0 gear_motor = 0, 5, 0 autopilot = 1, 5, 0 avionics_bus = 0, 10, 0 avionics = 1, 5, 0 pitot_heat = 0, 2, 0 additional_system = 0, 20, 0 marker_beacon = 1, 2, 0 gear_warning = 1, 2, 0 fuel_pump = 0, 5, 0 starter1 = 0, 20, 0 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 prop_sync = 0, 5, 17 auto_feather = 0, 15, 17 auto_brakes = 0, 15, 17 standby_vacuum = 0, 15, 17 hydraulic_pump = 0, 2, 17 fuel_transfer_pump = 0, 5, 17 propeller_deice = 0, 5, 17 light_recognition = 0, 5, 17 light_wing = 0, 5, 17 light_logo = 0, 5, 17 [pitot_static] vertical_speed_time_constant=100 [TailHook] tailhook_length=1 ;(feet) tailhook_position=0.0, 0.0, 0.0 ;(feet) longitudinal, lateral, vertical positions from datum cable_force_adjust=1.0 [exits] number_of_exits=2 exit_rate.0=0.4 ;Percent per second exit_rate.1=0.4 ;Percent per second [Views] eyepoint=-3.50,0.00,1.60 VIEW_FORWARD_ZOOM=0.75 [Reference Speeds] flaps_up_stall_speed=120.000 full_flaps_stall_speed=98.000 cruise_speed=354 max_indicated_speed=440.000000 max_mach=0.890 [autopilot] autopilot_available=0 flight_director_available=0 [Flaps.0] type=1 span-outboard=0.500 extending-time=5.000 system_type=1 damaging-speed=301 blowout-speed=405 lift_scalar=1.000 drag_scalar=1.000 pitch_scalar=1.000 flaps-position.0=0.000, 0.000 flaps-position.1=50, 0.000 tailwheel_lock=1 [brakes] toe_brakes_scale=0.125925 parking_brake=1 differential_braking_scale = 1.0 [gear_warning_system] gear_warning_available = 0 //Normal pct_throttle_limit = 0 //Percent throttle that activates warning flap_limit_idle = 0 //Flap angle that activates warning at idle flap_limit_power = 0 //Flap angle that activates warning at above idle [hydraulic_system] electric_pumps=0 engine_map=1,1,0,0 normal_pressure=1000.000000 [stall_warning] type=1 [attitude_indicators] attitude_indicator.0 = 1 [turn_indicators] turn_indicator.0=1,0 [direction_indicators] direction_indicator.0=1,0 [airspeed_indicators] airspeed_indicator.0=1,0 [Radios] Audio.1=1 Com.1=1,0 Adf.1=1,0 Transponder.1=1 Marker.1=1 [folding_wings] wing_fold_system_type = 4 ;0=None fold_rates = 10,10 ;Percent per second [flight_tuning] cruise_lift_scalar=1.0 parasite_drag_scalar=0.70 induced_drag_scalar=0.80 elevator_effectiveness=1.0 aileron_effectiveness=0.9 rudder_effectiveness=1.0 pitch_stability=1.5 roll_stability=1.5 yaw_stability=1.0 elevator_trim_effectiveness=1.0 aileron_trim_effectiveness=1.0 rudder_trim_effectiveness=1.0 hi_alpha_on_roll=1.0 hi_alpha_on_yaw=1.0 p_factor_on_yaw=1.0 torque_on_roll=1.0 gyro_precession_on_roll=1.0 gyro_precession_on_yaw=1.0
