[fltsim.0] title=VW-Racer sim=cessna172sp model="" panel="" sound="" texture= kb_checklists=Wright_Flyer_check kb_reference=Wright_Flyer_ref atc_id=N9FLY atc_id_color=0xffffffff ui_manufacturer=Volkswagon ui_type=Beatle ui_variation=Drag-car description= [General] atc_type=Wright Flyer atc_model="" editable=0 performance=\n [WEIGHT_AND_BALANCE] max_gross_weight=5650 // (pounds) empty_weight=1650 // (pounds) reference_datum_position=3.6, 0, 0 // (feet) distance from FlightSim Reference position: (1/4 chord, centerline, waterline) empty_weight_CG_position=-3.0, 0, 0 // (feet) longitudinal, lateral, vertical distance from specified datum max_number_of_stations=50 station_load.0="170, -3.0, -1.5, -2.0, " // Weight (lbs), longitudinal, lateral, vertical positions from datum (feet) station_load.1="170, -3.0, 1.5, -2.0, " // Weight (lbs), longitudinal, lateral, vertical positions from datum (feet) station_load.2="0, -6.2, -1.5, -2.0, " // Weight (lbs), longitudinal, lateral, vertical positions from datum (feet) station_load.3="0, -6.2, 1.5, -2.0, " // Weight (lbs), longitudinal, lateral, vertical positions from datum (feet) station_load.4="0, -8.0, 0.0, -2.0, " // Weight (lbs), longitudinal, lateral, vertical positions from datum (feet) ;Moments of Inertia empty_weight_pitch_MOI=5400.0 empty_weight_roll_MOI=5137.0 empty_weight_yaw_MOI=2360.0 empty_weight_coupled_MOI=0.0 [flight_tuning] cruise_lift_scalar=0.0 parasite_drag_scalar=1.0 induced_drag_scalar=1.0 elevator_effectiveness=0.0 aileron_effectiveness=0.0 rudder_effectiveness=0.1 pitch_stability=15.0 roll_stability=15.0 yaw_stability=15.0 elevator_trim_effectiveness=5.0 aileron_trim_effectiveness=1.0 rudder_trim_effectiveness=5.0 [GeneralEngineData] engine_type=0 //0=Piston, 1=Jet, 2=None, 3=Helo-Turbine, 4=Rocket, 5=Turboprop Engine.0=-6.4, 0.0, -3.0 //(feet) longitudinal, lateral, vertical distance from reference datum fuel_flow_scalar=0.88 //Fuel flow scalar min_throttle_limit=0.0 //Minimum percent throttle. Generally negative for turbine reverser [piston_engine] power_scalar=3.0 //Piston power scalar cylinder_displacement=90.3 //Cubic inches per cylinder compression_ratio=8.5 //Compression ratio number_of_cylinders=10 //Number of cylinders max_rated_rpm=5000 //Max rated RPM max_rated_hp=500 //Max rated HP fuel_metering_type=1 //0=Fuel Injected, 1=Gravity Carbureter, 2=Aerobatic Carbureter cooling_type=0 //0=Cooling type Air, 1=Cooling type Liquid normalized_starter_torque=0.3 //Starter torque factor turbocharged=0 //Is it turbocharged? 0=FALSE, 1=TRUE max_design_mp=0 //Max design manifold pressure, (inHg) min_design_mp=0 //Min design manifold pressure, (inHg) critical_altitude=0 //Altitude to which the turbocharger will provide max design manifold pressure (feet) emergency_boost_type=0 //0=None, 1=Water Injection, 2=Methanol/Water injection, 3=War Emergency Power emergency_boost_mp_offset=0 //Additional manifold pressure supplied by emergency boost emergency_boost_gain_offset=0 //Multiplier on manifold pressure due to emergency boost fuel_air_auto_mixture=0 //Automixture available? 0=FALSE, 1=TRUE auto_ignition=0 //Auto-Ignition available? 0=FALSE, 1=TRUE max_rpm_mechanical_efficiency_scalar=1.0 //Scalar on maximum RPM mechanical efficiency idle_rpm_mechanical_efficiency_scalar=1.0 //Scalar on idle RPM mechanical efficiency max_rpm_friction_scalar=1.0 //Scalar on maximum RPM friction idle_rpm_friction_scalar=1.0 //Scalar on idle RPM friction [propeller] thrust_scalar=1.0 //Propeller thrust scalar propeller_type=0 //0=Constant Speed, 1=Fixed Pitch propeller_diameter=6.8 //Propeller Diameter, (feet) propeller_blades=2 //Number of propeller blades propeller_moi=8.7 //Propeller moment of inertia beta_max=31.8 //Maximum blade pitch angle for constant speed prop, (degrees) beta_min=17.0 //Minimum blade pitch angle for constant speed prop, (degrees) min_gov_rpm=1400 //Miminum governed RPM prop_tc=0.1 //Prop time-constant gear_reduction_ratio=1.0 //Propeller gear reduction ratio fixed_pitch_beta=20 //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=0 //Prop de-icing available? 0=FALSE, 1=TRUE prop_feathering_available=0 //Prop feathering available? 0=FALSE, 1=TRUE prop_auto_feathering_available=0 //Prop auto-feathering available? 0=FALSE, 1=TRUE min_rpm_for_feather=0 //Minimum RPM for prop feathering beta_feather=0 //Feathering pitch angle (degrees) power_absorbed_cf=0 //Coefficient of friction for power absorbed by propeller defeathering_accumulators_available=0 //Defeathering accumulators available? 0=FALSE, 1=TRUE prop_reverse_available=0 //Prop reverse available? 0=FALSE, 1=TRUE minimum_on_ground_beta=0 //Miminum pitch angle on ground, (degrees) minimum_reverse_beta=0 //Minimum pitch angle in reverse, (degrees) [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 ;/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 [contact_points] point.0=1, 0.90, -2.61, -3.50, 1500, 0, 1.5, 30.0, 0.25,2.5, 0.7, 0.0, 0.0, 0 point.1=1, 0.90, 2.61, -3.50, 1500, 0, 1.5, 30.0, 0.25,2.5, 0.7, 0.0, 0.0, 0 point.2=1, -7.8, -2.65, -3.55, 3500, 1, 1.5, 0.0, 0.3, 2.5, 0.7, 0.0, 0.0, 2 point.3=1, -7.8 2.65, -3.55, 3500, 2, 1.5, 0.0, 0.3, 2.5, 0.7, 0.0, 0.0, 3 point.4=2, -3.90, -18.0, 3.00, 1800, 0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 5 point.5=2, -3.90 18.0, 3.00, 1800, 0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 6 point.6=2,-20.23, 0.0, 0.30, 1800, 0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 9 point.7=2, 1.48, 0.0, -2.17, 1800, 0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 4 point.8=2,-22.80, 0.0, 5.83, 1800, 0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 7 point.9=2, -4.90, 0.0, -2.00, 1800, 0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 8 max_number_of_points=21 static_pitch=3.02 //degrees, pitch when at rest on the ground (+=Up, -=Dn) static_cg_height=3.765 //feet, altitude of CG when at rest on the ground [brakes] parking_brake=1 //Parking brake available toe_brakes_scale=2.0 //Brake scalar [hydraulic_system] normal_pressure=0.0 //PSI [Views] eyepoint=-3.25, -1.15, 0.89 //(feet) longitudinal, lateral, vertical distance from reference datum [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.0=5, 2.8, -1.95, -1.34, fx_landing, light.1=5, 2.8, 1.95, -1.34, fx_landing, light.2=4, -3.25, 0.0, 0.89, fx_vclight, [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=1,0 [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=1,1 //Turn AND Bank [EFFECTS] //wake=fx_wake //water=fx_spray //dirt=fx_tchdrt //concrete=fx_sparks //touchdown=fx_tchdwn_s, 1 [fuel] LeftMain=-3.0, 0.0, -0.0, 139.0, 0.0 //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons) fuel_type=1 //Fuel type: 1 = Avgas, 2 = JetA number_of_tank_selectors=1 electric_pump=1 [airplane_geometry] wing_area=1.0 //Square feet wing_span=0.1 //Feet wing_root_chord=0.9 //Feet wing_dihedral=1.7 //Degrees wing_incidence=1.5 //Degrees wing_twist=-3.0 //Degrees oswald_efficiency_factor=0.68 //Measure of lift effeciency of wing wing_winglets_flag=0 //Are winglets available? wing_sweep=0 //Degrees, wing leading edge wing_pos_apex_lon=-2.4 //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=9.0 //Square feet htail_span=11.7 //Feet htail_pos_lon=-18.3 //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=3.2 //Degrees htail_sweep=10.0 //Degrees, horizontal tail leading edge vtail_area=18.0 //Square feet vtail_span=4.8 //Feet, tip to body vtail_sweep=40.0 //Degrees, vertical tail leading edge vtail_pos_lon=-16.2 //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=6.7 //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=34.0 //Degrees elevator_trim_limit=19.5 //Degrees spoiler_limit=15.0 //Degrees spoilerons_available=0 //Spoilerons Available? aileron_to_spoileron_gain=0 //Aileron to spoileron gain min_ailerons_for_spoilerons=0 //Degrees min_flaps_for_spoilerons=0 //Minimum flap handle position when spoilerons activate [flaps.0] type=1 // 1 - tail, 2 - lead span-outboard=0.5 // 0.0 .. 1.0 extending-time=7 // seconds flaps-position.0=0 // degrees flaps-position.1=12.7 // degrees flaps-position.2=25.3 // degrees flaps-position.3=38 // degrees damaging-speed=120 // KIAS blowout-speed=150 // KIAS lift_scalar=1.0 drag_scalar=1.0 pitch_scalar=1.0 system_type=0 //0=Electric, 1=Hydraulic, 2=Pneumatic, 3=Manual, 4=None [Reference Speeds] flaps_up_stall_speed=53.0 //Knots True (KTAS) full_flaps_stall_speed=48.0 //Knots True (KTAS) cruise_speed=115.0 //Knots True (KTAS) max_indicated_speed=163 //Red line (KIAS) [autopilot] autopilot_available=1 flight_director_available=0 default_vertical_speed=700.0 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=6000 ; 0 - 10000 gear_bump_nose_direction=18000 ; 0 - 35999 degrees gear_bump_nose_duration=250000 ; in microseconds gear_bump_left_magnitude=6000 ; 0 - 10000 gear_bump_left_direction=35500 ; 0 - 35999 degrees gear_bump_left_duration=250000 ; in microseconds gear_bump_right_magnitude=6000 ; 0 - 10000 gear_bump_right_direction=00500 ; 0 - 35999 degrees gear_bump_right_duration=250000 ; in microseconds ground_bumps_magnitude1=3250 ; 0 - 10000 ground_bumps_angle1=8900 ; 0 - 35999 degrees ground_bumps_intercept1=5.0 ground_bumps_slope1=0.48 ground_bumps_magnitude2=750 ; 0 - 10000 ground_bumps_angle2=9100 ; 0 - 35999 degrees ground_bumps_intercept2=0.075 ground_bumps_slope2=1.0 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=1 [exits] number_of_exits=2 exit_rate.0=0.2 ;Percent per second exit_rate.1=0.4 ;Percent per second