[fltsim.0] title=B-24J Liberator sim=B24j model= panel= sound= texture= ui_manufacturer=Consolidated ui_type=B-24 J ui_variation=B-24J-190 description=B-24 J-190 90 BG - 321 BS atc_heavy=0 atc_id= atc_airline= atc_flight_number= [fltsim.1] title=B-24J Liberator Paint1 sim=B24j model=1 panel= sound= texture= ui_manufacturer=Consolidated ui_type=B-24 J ui_variation=B-24J-5 description=B-24 J-5 "Delectable Doris" 389 BG - 566BS - 8AF atc_heavy=0 atc_id= atc_airline= atc_flight_number= [WEIGHT_AND_BALANCE] empty_weight= 37000.000 reference_datum_position= 0.000, 0.000, 0.000 empty_weight_CG_position= 6.500, 0.000, 0.000 max_number_of_stations=50 station_load.0= 170.000, 8.000, -4.000, 2.000 station_load.0=170, 8.0, 4.0, 2.0 //Co-Pilot Weight (lbs), longitudinal, lateral, vertical positions from datum (feet) ;Moments of Inertia empty_weight_pitch_MOI= 556044.000 empty_weight_roll_MOI= 1104581.000 empty_weight_yaw_MOI= 1130739.000 empty_weight_coupled_MOI= 0.000 max_gross_weight= 80418.000 CG_forward_limit= 0.000 CG_aft_limit= 1.000 [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=1.0 rudder_trim_effectiveness=1.0 [piston_engine] power_scalar=1.6 cylinder_displacement= 130.700 compression_ratio= 6.700 number_of_cylinders= 14 max_rated_rpm= 2700.000 max_rated_hp= 1200.000 fuel_metering_type= 0 cooling_type= 0 normalized_starter_torque= 0.035 turbocharged= 1 max_design_mp= 46.000 min_design_mp= 1.000 critical_altitude= 17000.000 emergency_boost_type= 0 emergency_boost_mp_offset= 0.000 emergency_boost_gain_offset= 0.000 fuel_air_auto_mixture= 0 auto_ignition= 0 max_rpm_mechanical_efficiency_scalar= 1.000 idle_rpm_mechanical_efficiency_scalar= 1.000 max_rpm_friction_scalar= 1.000 idle_rpm_friction_scalar= 1.000 [propeller] thrust_scalar=1.2 rotation= -1,1,-1,1 //Engine 1,2,3,... Rotation direction. 1 = CW, -1 = CCW propeller_type= 0 propeller_diameter= 12.000 propeller_blades= 2 propeller_moi= 34.000 beta_max= 65.000 beta_min= 18.000 min_gov_rpm= 1500.000 prop_tc= 0.010 gear_reduction_ratio= 1.350 fixed_pitch_beta= 0.000 low_speed_theory_limit= 80.000 prop_sync_available= 0 prop_deice_available= 0 prop_feathering_available= 0 prop_auto_feathering_available= 0 min_rpm_for_feather= 0.000 beta_feather= 0.000 power_absorbed_cf= 0.000 defeathering_accumulators_available= 0 prop_reverse_available= 0 minimum_on_ground_beta= 0.000 minimum_reverse_beta= 0.000 [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 point.0= 1.000, 15.500, 0.000, -8.800, 1400.000, 0.000, 1.500, 42.700, 1.060, 2.500, 0.700, 6.000, 7.000, 0.000, 0.000, 0.000 point.1= 1.000, -1.500, -13.170, -10.000, 2000.000, 1.000, 2.500, 0.000, 1.060, 2.500, 0.860, 7.500, 8.500, 2.000, 0.000, 0.000 point.2= 1.000, -1.500, 13.170, -10.000, 2000.000, 2.000, 2.500, 0.000, 1.060, 2.500, 0.860, 7.000, 8.000, 3.000, 0.000, 0.000 point.3= 2.000, 0.000, -55.830, 1.000, 800.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 5.000, 0.000, 0.000 point.4= 2.000, 0.000, 55.830, 1.000, 800.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 6.000, 0.000, 0.000 point.5= 2.000, -39.580, 0.000, -2.830, 800.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 9.000, 0.000, 0.000 point.6= 2.000, 17.160, 0.000, -4.830, 800.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 4.000, 0.000, 0.000 static_cg_height= 10.780 static_pitch= 1.810 [Views] eyepoint=4.177945,0.000000,5.254470 [exits] number_of_exits = 2 exit_rate.0 = 0.4 ;Percent per second exit_rate.1 = 0.4 [fuel] Center1= 2.000, 0.000, -1.170, 1600.000, 0.000 LeftMain= -2.330, -22.400, 0.230, 2804.000, 0.000 RightMain= -2.330, 22.400, 0.230, 2804.000, 0.000 fuel_type= 1.000 number_of_tank_selectors= 1 [airplane_geometry] wing_area= 1736.000 wing_span= 141.250 wing_root_chord= 12.250 wing_dihedral= 4.477 wing_incidence= 2.197 wing_twist= 0.000 oswald_efficiency_factor= 0.358 wing_winglets_flag= 0 wing_sweep= 0.000 wing_pos_apex_lon= 0.000 wing_pos_apex_vert= 0.000 htail_area= 356.000 htail_span= 43.417 htail_pos_lon= -60.083 htail_pos_vert= 0.000 htail_incidence= 2.000 htail_sweep= 0.000 vtail_area= 333.000 vtail_span= 20.806 vtail_sweep= 0.000 vtail_pos_lon= -52.750 vtail_pos_vert= 1.500 elevator_area= 183.080 aileron_area= 198.400 rudder_area= 116.550 elevator_up_limit= 27.502 elevator_down_limit= 20.626 aileron_up_limit= 25.210 aileron_down_limit= 25.210 rudder_limit= 24.637 elevator_trim_limit= 19.481 spoiler_limit= 0.573 spoilerons_available= 0 aileron_to_spoileron_gain= 0.000 min_ailerons_for_spoilerons= 0.000 min_flaps_for_spoilerons= 0.000 [GeneralEngineData] engine_type= 0 Engine.0= 10.083, -30.167, 1.917 Engine.1= 10.833, -14.500, -0.667 Engine.2= 10.833, 14.500, -0.667 Engine.3= 10.083, 30.167, 1.917 fuel_flow_scalar= 1.000 [Reference Speeds] flaps_up_stall_speed= 94.000 full_flaps_stall_speed= 75.200 cruise_speed= 212.086 [keyboard_response] elevator= 150.000, 250.000 aileron= 150.000, 250.000 rudder= 150.000, 250.000 [General] performance=Length: 67ft 2 ins\nSpan: 110 ft\s Wing area: 1048 sq ft\nWeight: empty 38,000 lb\s loaded 71,000 l\nPower:4 x P&W R-1830-65s of 1,200 hp\nRange: 1,700 miles with 5,000 lb bombs\nDate:January 2000\nDetails:Long range heavy bomber\nDesigner: Roger Lowery atc_type= atc_model= [autopilot] autopilot_available= 1 flight_director_available= 0 default_vertical_speed= 700.000 autothrottle_available= 1 autothrottle_arming_required= 1 autothrottle_takeoff_ga= 1 autothrottle_max_rpm= 90.000 pitch_takeoff_ga= 8.000 [Flaps.0] type= 1 span-outboard= 0.500 extending-time= 5.000 system_type= 0 damaging-speed= 0.000 blowout-speed= 0.000 lift_scalar= 1.000 drag_scalar= 1.000 pitch_scalar= 1.000 flaps-position.0= 0.000, 0.000 flaps-position.1= 7.998, 0.000 flaps-position.2= 15.997, 0.000 flaps-position.3= 23.995, 0.000 flaps-position.4= 31.994, 0.000 flaps-position.5= 39.992, 0.000 [direction_indicators] direction_indicator.0=1,0
