[fltsim.0] title=Liberty ship sim=liberty ship model= panel= sound= texture= checklists= ui_manufacturer=Ship ui_type=Sh_Liberty ship ui_variation=USS Navy [General] atc_type= atc_model= editable=1 performance=Maximum Speed\t20 kts\nCruise Speed\t11 kts\nMaximum Range\t19,000 nm\nService Ceiling\t0 ft\nFuel Capacity\t12,500 barrels\nMax Gross Weight\t20 million lbs\nSeating\t\t81\nUseful Load\t18 million lbs\n [Reference Speeds] flaps_up_stall_speed = 040 full_flaps_stall_speed = 000 cruise_speed = 020 max_indicated_speed = 040 max_mach = 0.10 [WEIGHT_AND_BALANCE] max_gross_weight = 875000 empty_weight = 401100 reference_datum_position = 0,0,0 ;ZXY distance from FlightSim Reference empty_weight_CG_position = 0,0,0 ;ZXY distance from specified datum max_number_of_stations = 10 station_load.0 = 40000, 0,0,0 ;Payload Weight, ZXY position from datum ;Moments of Inertia empty_weight_pitch_MOI = 96304110 ;originally 24223159 empty_weight_roll_MOI = 15352310 ;computed as 672647 empty_weight_yaw_MOI = 32167308 ;originally 39531785 empty_weight_coupled_MOI = 0 [contact_points] ; 0 Class (0=floats) ; 1 Longitudinal Position (feet) [BIGGER = SLOWER WAVE MOTION + NOSE PLOWS] ; 2 Lateral Position (feet) [BIGGER CREATES VIBRATION] ; 3 Vertical Position (feet) [MORE POSITIVE = LOWER] ; 4 Impact Damage Threshold (Feet Per Minute) ; 5 Brake Map (0=None, 1=Left, 2=Right) [N/A] ; 6 Wheel Radius (feet) ; 7 Steer Angle (degrees) [CHANGE THIS TO MAKE SHIP TURN FASTER] ; 8 Static Compression (feet) (0=rigid) ; 9 Max/Static Compression Ratio ;10 Damping Ratio/Water Rudder Effectiveness (0=Undamped, 1=Critically Damped) ;11 Extension Time (seconds) [N/A TO FIXED GEAR] ;12 Retraction Time (seconds) [N/A TO FIXED GEAR] ;13 Sound Type [WATER SOUND?] ;14 Airspeed limit for retraction (KIAS) [N/A TO FIXED GEAR] ;15 Airspeed that gear gets damage at (KIAS) [N/A TO FIXED GEAR] ; 0 1 2 3 4 5 6 7 8 9 10 11 12 13 14 15 ; 0 Z X Y FPM BM WR SA SC Max DR ET RT SND RL GD point.0=4, 40,-3.5, -3.5, 9999, 0, 1, 05, 0.9, 15.5, 0.65, 00, 00, 2, 00, 00 point.1=4, 40, 3.5, -3.5, 9999, 0, 1, 05, 0.9, 15.5, 0.65, 00, 00, 3, 00, 00 point.2=4,-40,-3.5, -3.5, 9999, 0, 1, 00, 0.9, 15.5, 0.65, 00, 00, 2, 00, 00 point.3=4,-40, 3.5, -3.5, 9999, 0, 1, 00, 0.9, 15.5, 0.65, 00, 00, 3, 00, 00 point.4=1, 0, 0, -4.0, 9999, 0, 1, 00, 0.9, 15.5, 0.65, 05, 05, 3, 00, 00 ;FOR HORN static_pitch = 0.0 static_cg_height = 4.0 ;[MUST BE POS #, OR FLIES INTO SPACE] gear_system_type = 0 ;Hydraulic [FOR HORN] [Views] eyepoint= 14.9, 0.0, 42.7 //eyepoint = 66.9, 0.0, 34.7 ;ZXY distance from reference datum (feet) [flight_tuning] cruise_lift_scalar = 1.000 ;changed from 1 to 0 parasite_drag_scalar = 1.000 induced_drag_scalar = 1.000 elevator_effectiveness = 1.000 ;changed from 1 to 0 aileron_effectiveness = 5.000 ;changed from 1 to 0 rudder_effectiveness = 1.000 ;changed from 1 to 0 pitch_stability = 1.000 roll_stability = 1.000 yaw_stability = 1.000 elevator_trim_effectiveness = 1.000 ;changed from 1 to 0 aileron_trim_effectiveness = 1.000 ;changed from 1 to 0 rudder_trim_effectiveness = 1.000 ;changed from 1 to 0 [airplane_geometry] ;[NO CHANGES] wing_area = 5825.0 ;Square feet wing_span = 211.4 wing_root_chord = 48.8 wing_dihedral = 7.0 ;Degrees wing_incidence = 2.0 ;Degrees wing_twist = -1.0 ;Degrees oswald_efficiency_factor = 0.68 ;Measure of lift effeciency of wing wing_winglets_flag = 1 ;Are winglets available? wing_sweep = 37.5 ;Degrees, wing leading edge wing_pos_apex_lon = -68.2 ;Z distance from ref point wing_pos_apex_vert = 0 ;Y distance from ref point htail_area = 1470 ;Square feet htail_span = 72.8 htail_pos_lon = -210.0 ;Z distance from ref point htail_pos_vert = 0.0 ;Y distance from ref point htail_incidence = 0.0 ;Degrees htail_sweep = 37.5 ;horizontal tail leading edge vtail_area = 1060 ;Square feet vtail_span = 37.1 ;tip to body vtail_sweep = 45.0 ;Degrees, vertical tail leading edge vtail_pos_lon = -198.5 ;Z distance from ref point vtail_pos_vert = 26.1 ;Y from ref point elevator_area = 327 ;Square feet aileron_area = 225 ;Square feet rudder_area = 230 ;Square feet elevator_up_limit = 25 ;Degrees elevator_down_limit = 15 ;Degrees aileron_up_limit = 25 ;Degrees aileron_down_limit = 15 ;Degrees rudder_limit = 21.5 ;Degrees elevator_trim_limit = 20 ;Degrees spoiler_limit = 45 ;Degrees spoilerons_available = 1 ;Spoilerons Available? aileron_to_spoileron_gain = 3 ;Aileron to spoileron gain min_ailerons_for_spoilerons = 10 ;Degrees min_flaps_for_spoilerons = 0 ;Minimum flap handle position when spoilerons activate ;[flaps.0] ;type = 0 [flaps.0] type = 1 ;(1 - tail) span-outboard = 0.8 ;0.0 .. 1.0 extending-time = 2 ;seconds flaps-position.0 = 0 ;degrees flaps-position.1 = 1 ;degrees damaging-speed = 120 ;KIAS blowout-speed = 150 ;KIAS lift_scalar = 0.0 drag_scalar = 0.0 pitch_scalar = 0.0 system_type = 1 ;(0=Electric) [GeneralEngineData] engine_type = 1 ;1=Jet Engine.0 = 0,0,0 ;ZXY distance from ref datum fuel_flow_scalar = 1.0 ;Scalar for fuel flow efficiency min_throttle_limit = -0.25 ;neg for turbine reverser [TurbineEngineData] fuel_flow_gain = 0.002 ;Gain on fuel flow inlet_area = 60.0 ;Square Feet, engine nacelle inlet area rated_N2_rpm = 29920 ;RPM, 2nd stage compressor rated value static_thrust = 260000 ;Lbs, max rated static thrust at SL afterburner_available = 0 ;Afterburner available? reverser_available = 1 ;Thrust reverser available? [jet_engine] thrust_scalar = 1.0 [fuel] Center1 = 0,0,0,50000,10 ;ZXY GAL MIN fuel_type = 2 ;2 = JetA number_of_tank_selectors = 1 electric_pump = 1 [electrical] electric_always_available = 1 [Radios] // Radio Type = availiable, standby frequency, has glide slope Audio.1 = 1 Com.1 = 1, 1 Com.2 = 1, 1 Nav.1 = 1, 1, 1 Nav.2 = 1, 1, 0 Adf.1 = 1 Transponder.1 = 1 Marker.1 = 1 [gear_warning_system] gear_warning_available = 0 [brakes] parking_brake = 0 ;Parking brake not available toe_brakes_scale = 0 ;Brake scalar [hydraulic_system] normal_pressure = 3000 ;PSI electric_pumps = 0 ;no electric pumps engine_map = 1,0,0,0 ;pumps on Eng1 [pitot_static] vertical_speed_time_constant = 1 ;Increasing this value will cause a more instantaneous reaction in the VSI [direction_indicators] direction_indicator.0 = 3,0 ;3=Electro-Mag Slaved Compass, 0=NA [attitude_indicators] attitude_indicator.0 = 0 ;0=None [turn_indicators] turn_indicator.0 = 1,0 ;1=Electric Gyro [stall_warning] type = 0 [exits] number_of_exits=1 exit_rate.0=0.4 ;Percent per second [autopilot] autopilot_available= 1 flight_director_available= 1 default_vertical_speed= 1000.0 autothrottle_available=1 autothrottle_arming_required=1 autothrottle_max_rpm = 90 autothrottle_takeoff_ga=1 pitch_takeoff_ga=8.0 max_pitch=10.0 max_pitch_acceleration=1.0 max_pitch_velocity_lo_alt=2.0 max_pitch_velocity_hi_alt=1.5 max_pitch_velocity_lo_alt_breakpoint=20000.0 max_pitch_velocity_hi_alt_breakpoint=28000.0 max_bank=25.0 max_bank_acceleration=1.8 max_bank_velocity=3.00 max_throttle_rate=0.10 nav_proportional_control=9.00 nav_integrator_control=0.25 nav_derivative_control=0.00 nav_integrator_boundary=2.50 nav_derivative_boundary=0.00 gs_proportional_control=9.52 gs_integrator_control=0.26 gs_derivative_control=0.00 gs_integrator_boundary=0.70 gs_derivative_boundary=0.00 yaw_damper_gain = 0.0 [keyboard_response] ;Breakpoint speeds (knots) on the keyboard increments of control surfaces. ;Speed at which the incremenet is reduced to 1/2 and 1/8 respectively. elevator = 150, 250 aileron = 150, 250 rudder = 150, 250 [forcefeedback] ;revised to eliminate bumps gear_bump_nose_magnitude = 3000 ;0 - 10000 gear_bump_nose_direction = 18000 ;0 - 35999 degrees gear_bump_nose_duration = 250000 ;in microseconds gear_bump_left_magnitude = 2700 ;0 - 10000 gear_bump_left_direction = 35500 ;0 - 35999 degrees gear_bump_left_duration = 250000 ;in microseconds gear_bump_right_magnitude = 2700 ;0 - 10000 gear_bump_right_direction = 00500 ;0 - 35999 degrees gear_bump_right_duration = 250000 ;in microseconds ground_bumps_magnitude1 = 1300 ;0 - 10000 ground_bumps_angle1 = 08900 ;0 - 35999 degrees ground_bumps_intercept1 = 3.0 ground_bumps_slope1 = 0.20 ground_bumps_magnitude2 = 200 ;0 - 10000 ground_bumps_angle2 = 09100 ;0 - 35999 degrees ground_bumps_intercept2 = 1.075 ground_bumps_slope2 = 0.035 crash_magnitude1 = 10000 ;0 - 10000 crash_direction1 = 01000 ;0 - 35999 degrees crash_magnitude2 = 10000 ;0 - 10000 crash_direction2 = 9000 ;0 - 35999 degrees crash_period2 = 75000 ;in microseconds crash_duration2 = 2500000 ;in microseconds [EFFECTS] wake = fx_wake_ijt1 water =fx_spray_ijt1 wake=fx_wake_m water=fx_spray_seikan dirt=fx_tchdrt concrete=fx_sparks touchdown=fx_tchdwn_s, 1 [LIGHTS] ;type, Z, X, Y, effect ;Light types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing, 6=taxi, 7=recognition, 8=wing, 9=logo ;---internal (bridge) //light.1 = 4, 68.000, 0.000, 35.000, fx_navred ;night light ;---external light.2 = 3, 22.300,-28.000, 30.400, fx_navredh ;bridge left light.3 = 3, 22.300, 28.000, 30.400, fx_navgreh ;bridge right light.4 = 3, 60.900, 0.000, 75.999, fx_navwhih ;mainmast light.5 = 3,-108.850, 0.000, 75.999, fx_navwhih ;mizzenmast light.6 = 2, 0.150, 0.000,-59.500, fx_Smoke_asuka.fx light.7 = 2, 2.150, 0.000,-57.500, fx_Smoke_asuka.fx [SMOKESYSTEM] ;Press "I" to activate Y-not work, Z, X smoke.1 = 0.00,-120.0,-5.00, fx_spray1.fx ;prop smoke.2 = 0.00,-120.0, 5.00, fx_spray1.fx ;prop smoke.3 = 0.00, 132.0, 0.400, fx_ConstEXTRAeffects.fx, smoke.4 = 0.00, 40.0,-10.400, cannonfire.fx smoke.5=0.0, 6750.00,0.00, fx_ShellHit smoke.6=0.0,-6750.00,1100.00, fx_ShellHit
