[fltsim.0] title = 1GR Ta-152H-1 sim=tank152 model= panel= sound= texture= KB_checklists = CheckList_Ta-152H-1 ui_manufacturer=Lw ui_type=Focke Wulf ui_variation=TA 152 H-1%KeDI description=original by:n714VFTS & William Tell© Competition Certified atc_airline= atc_id=5 atc_flight_number= [WEIGHT_AND_BALANCE] empty_weight = 8979 reference_datum_position = 3.2, 0, 0 // (feet) distance from FlightSim Reference position: (1/4 chord, centerline, waterline) empty_weight_CG_position = -3.205, 0, 0 // (feet) longitudinal, lateral, vertical distance from specified datum max_number_of_stations = 50 station_load.0 = 220, -3.0, 0.0, 0.0 //Pilot Weight (lbs), longitudinal, lateral, vertical positions from datum (feet) ;Moments of Inertia empty_weight_pitch_MOI = 11395 empty_weight_roll_MOI = 11488 empty_weight_yaw_MOI = 21390 empty_weight_coupled_MOI=0.000000 max_gross_weight=13798.500000 [flight_tuning] cruise_lift_scalar = 1.0 parasite_drag_scalar = 1.0 induced_drag_scalar = 1.0 elevator_effectiveness = 1.5 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 = 1.0 rudder_trim_effectiveness = 1.0 [piston_engine] power_scalar = 1.0 cylinder_displacement=178.000000 compression_ratio=6.500000 number_of_cylinders=12 max_rated_rpm=3250.000000 max_rated_hp=1750.000000 fuel_metering_type=0 cooling_type=1 normalized_starter_torque=0.035000 turbocharged=1 max_design_mp=40.399999 min_design_mp=9.000000 critical_altitude=41010.000000 emergency_boost_type=2 emergency_boost_mp_offset=4.210000 emergency_boost_gain_offset=0.810055 fuel_air_auto_mixture=1 auto_ignition=0 max_rpm_mechanical_efficiency_scalar=1.000000 idle_rpm_mechanical_efficiency_scalar=1.000000 max_rpm_friction_scalar=1.000000 idle_rpm_friction_scalar=1.000000 [propeller] thrust_scalar = 1.0 propeller_type=0 propeller_diameter=10.833000 propeller_blades=2 propeller_moi=25.549361 beta_max=65.000000 beta_min=15.000000 min_gov_rpm=487.500000 prop_tc=0.010000 gear_reduction_ratio=2.398000 fixed_pitch_beta=20.000000 low_speed_theory_limit=80.000000 prop_sync_available=0 prop_deice_available=1 prop_feathering_available=1 prop_auto_feathering_available=0 min_rpm_for_feather=700.000000 beta_feather=88.500000 power_absorbed_cf=0.900000 defeathering_accumulators_available=1 prop_reverse_available=0 minimum_on_ground_beta=1.000000 minimum_reverse_beta=-14.000000 feathering_switches = 1 [exits] number_of_exits = 1 exit_rate.0 = 0.4 ;Percent per second [electrical] max_battery_voltage = 24.0 generator_alternator_voltage = 28.0 max_generator_alternator_amps = 60.0 [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 //14 Airspeed limit for retraction (KIAS) //15 Airspeed that gear gets damage at (KIAS) point.0= 1, -20.60, 0.00, -3.10, 3200, 0, 0.40,012.0, 0.30, 2.5, 0.70, 8.0, 9.0, 0, 0, 200 point.1= 1, 2.38, -5.74, -8.25, 2200, 1, 1.30, 0.0, 0.80, 2.5, 0.68, 5.0, 6.0, 2, 0, 200 point.2= 1, 2.38, 5.74, -8.25, 2200, 2, 1.30, 0.0, 0.80, 2.5, 0.68, 5.0, 5.0, 3, 0, 200 point.3= 2, 0.00,-17.25, -1.25, 1200, 0, 0.00, 0.0, 0.00, 0.0, 0.00, 0.0, 0.0, 5 point.4= 2, 0.00, 17.25, -1.25, 1200, 0, 0.00, 0.0, 0.00, 0.0, 0.00, 0.0, 0.0, 6 point.5= 2, -20.00, 0.00, 1.00, 2400, 0, 0.00, 0.0, 0.00, 0.0, 0.00, 0.0, 0.0, 9 point.6= 2, 2.41, 0.00, -2.08, 1200, 0, 0.00, 0.0, 0.00, 0.0, 0.00, 0.0, 0.0, 4 // point.0=1, -19.00, 0.00, -3.98, 3200, 0, 0.40,180.0, 0.30, 2.5, 0.70, 1.0, 6.0, 0, 0, 135 // point.1=1, 2.25, -5.60, -8.15, 2200, 1, 1.30, 0.0, 0.80, 2.5, 0.68, 5.0, 7.5, 2, 0, 135 // point.2=1, 2.25, 5.60, -8.15, 2200, 2, 1.30, 0.0, 0.80, 2.5, 0.68, 5.0, 7.5, 3, 0, 135 static_cg_height = 6.35 //(feet) altitude of CG when at rest (altitude when loaded on ground) static_pitch = 11.75 //degrees (pitch when loaded on ground) gear_system_type=1 [flaps.0] type=1 // 1 - tail, 2 - lead span-outboard=0.12 // 0.0 .. 1.0 extending-time=5 // seconds flaps-position.0=0 // degrees, KIAS flaps-position.1=24,205 // degrees, KIAS flaps-position.2=60,185 // degrees, KIAS // degrees, KIAS damaging-speed=205 // KIAS blowout-speed=220 // KIAS [Views] eyepoint=-5.0,0.00,2.49 [General] performance=Weight: 9179 lbs\nPower: 1750 hp\n9.0g Corner speed: 286 mph\nMax speed @ SL: 350 mph\nMax speed: 472 mph @ 41010 ft\nClimb rate: 3445 ft\/min @ 152 mph\nFlight Model By: gregoryp\n10\/18\/02 12:22 PM\nFlight Model Workbook V2.80.57 [fuel] LeftMain= -2, 0,-1.200000,62.0,0.0 RightMain= 2, 0,-1.200000,83.0,0.0 LeftAux= 0,-10, 0.200000,15.6,0.0 RightAux= 0,-10, 0.200000,15.6,0.0 fuel_type=1.000000 number_of_tank_selectors=1 electric_pump=1 [airplane_geometry] wing_area=251.000000 wing_span=47.416667 wing_root_chord=5.333333 wing_dihedral=6.998291 wing_incidence=0.999756 wing_twist=0.000000 oswald_efficiency_factor=0.882141 wing_winglets_flag=0 wing_sweep=0.000000 wing_pos_apex_lon=-3.200000 wing_pos_apex_vert=0.000000 htail_area=28.000000 htail_span=18.916667 htail_pos_lon=-22.533333 htail_pos_vert=0.000000 htail_incidence=0.000000 htail_sweep=0.000000 vtail_area=13.000000 vtail_span=4.110961 vtail_sweep=0.000000 vtail_pos_lon=-22.533333 vtail_pos_vert=7.083333 elevator_area=19.000000 aileron_area=23.000000 rudder_area=10.300000 elevator_up_limit=31.000000 elevator_down_limit=26.000000 aileron_up_limit=17.000000 aileron_down_limit=17.000000 rudder_limit=16.000000 elevator_trim_limit=18.000000 spoiler_limit=0.000000 spoilerons_available=0 aileron_to_spoileron_gain=0.000000 min_ailerons_for_spoilerons=0.000000 min_flaps_for_spoilerons=0.000000 [GeneralEngineData] engine_type=0 Engine.0=6.383333,0.000000,0.000000 fuel_flow_scalar=1.000000 min_throttle_limit=0.000000 [Reference Speeds] flaps_up_stall_speed=101.000000 full_flaps_stall_speed=80.800000 cruise_speed=284.604299 max_indicated_speed=439.117188 [keyboard_response] elevator=350.000000,500.000000 aileron=450.000000,1000.000000 rudder=200.000000,1000.000000 [autopilot] autopilot_available=1 flight_director_available=0 default_vertical_speed=700.000000 autothrottle_available=0 pitch_takeoff_ga=8.000000 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 [direction_indicators] direction_indicator.0=1,0 [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 = 500 gear_bump_right_duration = 250000 ground_bumps_magnitude1 = 3250 ground_bumps_angle1 = 8900 ground_bumps_intercept1 = 5# ground_bumps_slope1 = 0.48 ground_bumps_magnitude2 = 750 ground_bumps_angle2 = 9100 ground_bumps_intercept2 = 0.075 ground_bumps_slope2 = 1# crash_magnitude1 = 10000 crash_direction1 = 1000 crash_magnitude2 = 10000 crash_direction2 = 9000 crash_period2 = 75000 crash_duration2 = 2500000 [brakes] toe_brakes_scale=0.640889 parking_brake=1 [gear_warning_system] gear_warning_available=0 pct_throttle_limit=0.000000 flap_limit_power=0.000000 flap_limit_idle=0.000000 [hydraulic_system] electric_pumps=0 engine_map=1,0,0,0 normal_pressure=6.930556 [stall_warning] type=1 [attitude_indicators] attitude_indicator.0=1 [turn_indicators] turn_indicator.0=1,0
