[fltsim.0] title=MB-AI Submarino S30 sim=AI Submarino model= panel= sound= texture=S30 atc_id= atc_id_enable=1 atc_id_color=0xffffffff atc_airline=Marinha atc_flight_number= atc_heavy=0 ui_manufacturer=MB-AI ui_type=Submarino Classe Tupi/IKL 209 ui_variation=Tupi - S 30 visual_damage=0 atc_parking_types=DOCK atc_parking_codes=S description= Código Internacional de Chamada: PWTU. S Tupi - S 30 - Classe Tupi/IKL 209. Dimensões: 61.20 m de comprimento, 6.20 m de boca (7.60, incluindo os hidroplanos da popa) e 5.50 m de calado. Tripulação: 33 homens. [fltsim.1] title=MB-AI Submarino S31 sim=AI Submarino model= panel= sound= texture=S31 atc_id= atc_id_enable=1 atc_id_color=0xffffffff atc_airline=Marinha atc_flight_number= atc_heavy=0 ui_manufacturer=MB-AI ui_type=Submarino Classe Tupi/IKL 209 ui_variation=Tamoio - S 31 visual_damage=0 atc_parking_types=DOCK atc_parking_codes=S description= Código Internacional de Chamada: PWTA. S Tamoio - S 31 - Classe Tupi/IKL 209. Dimensões: 61.20 m de comprimento, 6.20 m de boca (7.60, incluindo os hidroplanos da popa) e 5.50 m de calado. Tripulação: 36 homens, sendo 7 oficiais e 29 suboficiais, sargentos, cabos e marinheiros. [fltsim.2] title=MB-AI Submarino S32 sim=AI Submarino model= panel= sound= texture=S32 atc_id= atc_id_enable=1 atc_id_color=0xffffffff atc_airline=Marinha atc_flight_number= atc_heavy=0 ui_manufacturer=MB-AI ui_type=Submarino Classe Tupi/IKL 209 ui_variation=Timbira - S 32 visual_damage=0 atc_parking_types=DOCK atc_parking_codes=S description= Código Internacional de Chamada: PWTI. S Timbira - S 32 - Classe Tupi/IKL 209. Dimensões: 61.20 m de comprimento, 6.20 m de boca (7.60, incluindo os hidroplanos da popa) e 5.50 m de calado. Tripulação: 33 homens. [fltsim.3] title=MB-AI Submarino S33 sim=AI Submarino model= panel= sound= texture=S33 atc_id= atc_id_enable=1 atc_id_color=0xffffffff atc_airline=Marinha atc_flight_number= atc_heavy=0 ui_manufacturer=MB-AI ui_type=Submarino Classe Tupi/IKL 209 ui_variation=Tapajó - S 33 visual_damage=0 atc_parking_types=DOCK atc_parking_codes=S description= Código Internacional de Chamada: PWTP. S Tapajó - S 33 - Classe Tupi/IKL 209. Dimensões: 61.20 m de comprimento, 6.20 m de boca (7.60, incluindo os hidroplanos da popa) e 5.50 m de calado. Tripulação: 33 homens. [fltsim.4] title=MB-AI Submarino S34 sim=AI Submarino model= panel= sound= texture=S34 atc_id= atc_id_enable=1 atc_id_color=0xffffffff atc_airline=Marinha atc_flight_number= atc_heavy=0 ui_manufacturer=MB-AI ui_type=Submarino Classe Tupi/IKL 209 ui_variation=Tikuna - S 34 visual_damage=0 atc_parking_types=DOCK atc_parking_codes=S description= S Tikuna - S 34 - Classe Tupi/IKL 209. Dimensões: 61.20 m de comprimento, 6.20 m de boca (7.60, incluindo os hidroplanos da popa) e 5.50 m de calado. Tripulação: 33 homens. [General] atc_type=MARINHA BRASILEIRA atc_model=Submarino editable=0 performance= \n \n \n \n \n \n \n [WEIGHT_AND_BALANCE] max_gross_weight=8000 // (pounds) empty_weight=4895 // (pounds) reference_datum_position=61.0, 0, 0 // (feet) distance from FlightSim Reference position: (1/4 chord, centerline, waterline) empty_weight_CG_position=-120.5, 0, 0 // (feet) longitudinal, lateral, vertical distance from specified datum max_number_of_stations=50 ;Moments of Inertia empty_weight_pitch_MOI=60000.00 empty_weight_roll_MOI=6618.57 empty_weight_yaw_MOI=10431.43 empty_weight_coupled_MOI=0.0 [Flaps.0] type=1 span-outboard=0.5 // Percent span for flap position extending-time=5.7 // Seconds, time to fully extend system_type=0 // 0 = electrical damaging-speed=175 // KIAS blowout-speed=175 // KIAS flaps-position.0=0 // degrees flaps-position.1=10,175 // degrees flaps-position.2=20,150 // degrees flaps-position.3=30,125 // degrees [flight_tuning] cruise_lift_scalar=0 parasite_drag_scalar=0 induced_drag_scalar=0 elevator_effectiveness=0 aileron_effectiveness=0 rudder_effectiveness=1.0 pitch_stability=0 roll_stability=1.0 yaw_stability=1.0 elevator_trim_effectiveness=0 aileron_trim_effectiveness=0 rudder_trim_effectiveness=1.0 [GeneralEngineData] engine_type=5 //0=Piston, 1=Jet, 2=None, 3=Helo-Turbine, 4=Rocket, 5=Turboprop Engine.0=-1.3, 0.0, 0.0 //(feet) longitudinal, lateral, vertical distance from reference datum fuel_flow_scalar=1.12 //Scalar for fuel flow efficiency min_throttle_limit=-0.25 //Minimum percent throttle. Generally negative for turbine reverser [propeller] thrust_scalar=1.0 //Propeller thrust scalar propeller_type=0 //0=Constant Speed, 1=Fixed Pitch propeller_diameter=8.8 //Propeller Diameter, (feet) propeller_blades=3 //Number of propeller blades propeller_moi=19 //Propeller moment of inertia beta_max=45 //Maximum blade pitch angle for constant speed prop, (degrees) beta_min=15.6 //Minimum blade pitch angle for constant speed prop, (degrees) min_gov_rpm=25520 //Miminum governed RPM prop_tc=0.004 //Prop time-constant gear_reduction_ratio=17.4 //Propeller gear reduction ratio fixed_pitch_beta=0 //Fixed pitch angle of fixed pitch prop, (degrees) low_speed_theory_limit=80 //Speed at which low speed theory becomes blended in (feet/second) prop_sync_available=0 //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=1 //Prop auto-feathering available? 0=FALSE, 1=TRUE min_rpm_for_feather=700 //Minimum RPM for prop feathering beta_feather=88.0 //Feathering pitch angle (degrees) power_absorbed_cf=0.9 //Coefficient of friction for power absorbed by propeller defeathering_accumulators_available=0 //Defeathering accumulators available? 0=FALSE, 1=TRUE prop_reverse_available=1 //Prop reverse available? 0=FALSE, 1=TRUE minimum_on_ground_beta=1.0 //Miminum pitch angle on ground, (degrees) minimum_reverse_beta=-14.0 //Minimum pitch angle in reverse, (degrees) [TurbineEngineData] fuel_flow_gain=0.011 //Gain on fuel flow inlet_area=1.0 //Square Feet, engine nacelle inlet area rated_N2_rpm=33000 //RPM, second stage compressor rated value static_thrust=158 //Lbs, max rated static thrust at Sea Level [turboprop_engine] power_scalar=0.85 //Scalar on Turboprop power maximum_torque=1865 //Maximum torque available (ft-lbs) [electrical] ;BusType, MaxAmpLoad, MinVoltage BusTypes:0=MainBus,1=AvionicsBus,2=BatteryBus,3=HotBatteryBus,4-7=Generator/AlternatorBus(1-4) flap_motor=0, 5 , 17.0 gear_motor=0, 5 , 17.0 autopilot=0, 5 , 17.0 avionics_bus=0, 5 , 17.0 avionics=1, 5 , 17.0 pitot_heat=0, 2 , 17.0 additional_system=0, 2 , 17.0 marker_beacon=1, 2 , 17.0 gear_warning=0, 2 , 17.0 fuel_pump=0, 5 , 17.0 starter1=0, 20, 17.0 light_nav=0, 5 , 17.0 light_beacon=0, 5 , 17.0 light_landing=0, 5 , 17.0 light_taxi=0, 5 , 17.0 light_strobe=0, 5 , 17.0 light_panel=0, 5 , 17.0 [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 / Water Rudder Effectiveness (0=Undamped, 1=Critically Damped) / 1.0 = normal ;/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, -11.15, 0.00, -5.300, 1600, 0, 1.40, 30.0, 0.3, 2.5, 0.8, 0.0, 0.0, 0, 175.0, 175.0 point.1=1, -124.40, -5.250, -5.500, 1600, 1, 1.50, 0.0, 0.4, 2.5, 0.8, 0.0, 0.0, 2, 175.0, 175.0 point.2=1, -124.40, 5.250, -5.500, 1600, 2, 1.50, 0.0, 0.4, 2.5, 0.8, 0.0, 0.0, 2, 175.0, 175.0 point.3=4, -37.0, -4.5, -6.0, 1000.0, 0, 2.0, 0.0, 0.5, 3.5, 0.900, 0.0, 0.0, 0, 220, 250 point.4=4, -37.0, 4.5, -6.0, 1000.0, 0, 2.0, 0.0, 0.5, 3.5, 0.900, 0.0, 0.0, 0, 220, 250 point.5=4, -121.0, -5.0, -2.3, 2000.0, 1, 2.0, 10.0, 1.0, 2.5, 0.900, 0.0, 0.0, 2, 220, 250 point.6=4, -121.0, 5.0, -2.3, 2000.0, 2, 2.0, 10.0, 1.0, 2.5, 0.900, 0.0, 0.0, 3, 220, 250 max_number_of_points=21 static_pitch=0.983 //degrees, pitch when at rest on the ground (+=Up, -=Dn) static_cg_height=5.344 //feet, altitude of CG when at rest on the ground gear_system_type=1 //Hydraulic [gear_warning_system] gear_warning_available=2 //Amphib pct_throttle_limit=0.1 //Percent throttle that activates warning flap_limit_idle=20.1 //Flap angle that activates warning at idle flap_limit_power=13.0 //Flap angle that activates warning at above idle [brakes] parking_brake=1 //Parking brake available toe_brakes_scale=0.68 //Brake scalar [hydraulic_system] normal_pressure=3000.0 //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, 1 Com.2=1, 1 Nav.1=1, 1, 1 Nav.2=1, 1, 0 Adf.1=1 Transponder.1=1 Marker.1=1 [LIGHTS] ;/Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit light.4=1, 25.00, 0.00, -6.00,fx_Ship_wake_2, [EFFECTS] wake=fx_wake_m water=fx_spray1 dirt=fx_tchdrt concrete=fx_AI_smoke_Tupi touchdown=fx_tchdwn_s, 1 [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=100, 180 aileron=200, 1000 rudder=200, 1000 [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=3,0 [attitude_indicators] ;/Type: 0=None, 1=Vacuum Gyro, 2=Electric Gyro attitude_indicator.0=1 [turn_indicators] ;/Type: 0=None, 1=Electric Gyro, 2=Vacuum Gyro turn_indicator.0=1,0 [airspeed_indicators] airspeed_indicator.0=1.16, -22.0 [exits] number_of_exits=2 exit_rate.0=0.4 ;Percent per second exit_rate.1=0.4 ;Percent per second [fuel] LeftMain=-15.3, -1.1, 2.5, 166.0, 3.6 //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons) RightMain=-15.3, 1.1, 2.5, 166.0, 3.6 //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons) fuel_type=2 //Fuel type: 1 = Avgas, 2 = JetA number_of_tank_selectors=1 electric_pump=1 [airplane_geometry] wing_area=279.0 //Square feet wing_span=52.1 //Feet wing_root_chord=6.4 //Feet wing_dihedral=3.9 //Degrees wing_incidence=2.5 //Degrees wing_twist=-1.7 //Degrees oswald_efficiency_factor=0.7 //Measure of lift effeciency of wing wing_winglets_flag=0 //Are winglets available? wing_sweep=2.96 //Degrees, wing leading edge wing_pos_apex_lon=-12.3 //Feet, longitudinal distance from reference point, negative going aft wing_pos_apex_vert=0.0 //Feet, vertical distance from reference point, positive going up htail_area=39.0 //Square feet htail_span=11.7 //Feet htail_pos_lon=-27.8 //Feet, longitudinal distance from reference point, negative going aft htail_pos_vert=0.0 //Feet, vertical distance from reference point, positive going up htail_incidence=2.0 //Degrees htail_sweep=5.0 //Degrees, horizontal tail leading edge vtail_area=18.0 //Square feet vtail_span=4.8 //Feet, tip to body vtail_sweep=45.0 //Degrees, vertical tail leading edge vtail_pos_lon=-25.7 //Feet, longitudinal distance from reference point, negative going aft vtail_pos_vert=1.5 //Feet, vertical distance from reference point, positive going up elevator_area=16.6 //Square feet aileron_area=18.3 //Square feet rudder_area=6.6 //Square feet elevator_up_limit=28.0 //Degrees elevator_down_limit=21.0 //Degrees aileron_up_limit=20.0 //Degrees aileron_down_limit=15.0 //Degrees rudder_limit=15.5 //Degrees elevator_trim_limit=19.5 //Degrees spoiler_limit=20.0 //Degrees spoilerons_available=1 //Spoilerons Available? aileron_to_spoileron_gain=1 //Aileron to spoileron gain min_ailerons_for_spoilerons=0 //Degrees min_flaps_for_spoilerons=0 //Minimum flap handle position when spoilerons activate spoiler_handle_available=0 //Defaults to True if spoiler limit > 0, else False. Should be False for spoilerons only [Reference Speeds] flaps_up_stall_speed=72.0 //Knots True (KCAS) full_flaps_stall_speed=58.0 //Knots True (KCAS) cruise_speed=143.0 //Knots True (KTAS) max_mach=0.60 max_indicated_speed=175 //Red line (KIAS) [autopilot] autopilot_available=1 flight_director_available=1 default_vertical_speed=1000.0 autothrottle_available=0 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 [forcefeedback] 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 [stall_warning] type=2 [Views] eyepoint=-36.100000,0.000000,0.000000
