[fltsim.0] title=Austflight Drifter Wires sim=Drifter model=wires panel= sound= texture= kb_checklists= kb_reference= atc_id=1458 atc_id_color=0xffffffff ui_manufacturer=Austflight ui_type=Drifter ui_variation=Flying Wires visual_damage=1 atc_heavy=0 atc_airline= atc_flight_number= description=\n The Drifter is a two seater aircraft that is certified in the primary category by the Civil Aviation Safety Authority, Australia. The Drifter has been operating in Australia since the early 1980s with approximately 500 built and sold. The aircraft has undergone several phases of development and some aircraft in the field are now approaching 10,000 hours of operation. The aircraft has a long history of safe operation and has a reputation of being reliable, economical and robust. The Drifter is manufactured by an Australian company, Drifter Aircraft Pty Ltd in Queensland, Australia [fltsim.1] title=Austflight Drifter Rigid Struts sim=Drifter model=rigid panel= sound= texture= kb_checklists= kb_reference= atc_id=1458 atc_id_color=0xffffffff ui_manufacturer=Austflight ui_type=Drifter ui_variation=Rigid Struts visual_damage=1 atc_heavy=0 atc_airline= atc_flight_number= description=\n The Drifter is a two seater aircraft that is certified in the primary category by the Civil Aviation Safety Authority, Australia. The Drifter has been operating in Australia since the early 1980s with approximately 500 built and sold. The aircraft has undergone several phases of development and some aircraft in the field are now approaching 10,000 hours of operation. The aircraft has a long history of safe operation and has a reputation of being reliable, economical and robust. The Drifter is manufactured by an Australian company, Drifter Aircraft Pty Ltd in Queensland, Australia [General] atc_type=Austflight atc_model=Drifter editable=1 performance=Maximum Speed\t\n80 kts \n\nEngine \t\nRotax 503\n\nMaximum Range\t\n 2.5 Hrs\n\nService Ceiling\t\n9,500 ft \n\nLength\t\n18.9 ft \n\nWingspan\t\n30 ft\n\nHeight\t\n108 in \n\nSeating\t\n2\n [WEIGHT_AND_BALANCE] max_gross_weight = 880.000 empty_weight = 448.580 reference_datum_position = 0.000, 0.000, 0.000 empty_weight_CG_position = 1.000, 0.000, 0.000 max_number_of_stations =50 station_load.0=170, -1.485, 0.0, 2.292 //Pilot Weight (lbs), longitudinal, lateral, vertical positions from datum (feet) station_load.1=120, -1.485, 0.0, -0.989 //Front Passenger Weight (lbs), longitudinal, lateral, vertical positions from datum (feet) ;Moments of Inertia empty_weight_pitch_MOI=672.0 empty_weight_roll_MOI=537.0 empty_weight_yaw_MOI=760.0 CG_forward_limit=1.000000 CG_aft_limit=-1.000000 empty_weight_coupled_MOI=0.000000 [flight_tuning] cruise_lift_scalar =1.8 parasite_drag_scalar =1.0 induced_drag_scalar =1.0 elevator_effectiveness =1.0 aileron_effectiveness =1.0 rudder_effectiveness =2.0 elevator_trim_effectiveness =1.0 aileron_trim_effectiveness =1.0 rudder_trim_effectiveness =1.0 pitch_stability =1.0 roll_stability =1.0 yaw_stability =1.0 hi_alpha_on_roll = 1.0 //At high AoA hi_alpha_on_yaw = 1.0 //At high AoA p_factor_on_yaw = 1.0 //Prop induced torque_on_roll = 0.5 //Prop induced gyro_precession_on_roll = 0.5 //Prop induced gyro_precession_on_yaw = 0.5 //Prop induced [piston_engine] power_scalar = 1.0 //Piston power scalar cylinder_displacement= 44.0 //Cubic inches per cylinder compression_ratio= 7.50 //Compression ratio number_of_cylinders=2 //Number of cylinders max_rated_rpm= 6800.00 //Max rated RPM max_rated_hp= 49.6 //Max rated HP fuel_metering_type= 1 //0=Fuel Injected, 1=Gravity Carburetor, 2=Aerobatic Carburetor cooling_type= 0 //0=Cooling type Air, 1=Cooling type Liquid normalized_starter_torque= 1.300 //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 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= 0.2 //Scalar on idle RPM friction [propeller] thrust_scalar = 1.5 //Propeller thrust scalar propeller_type= 1 //0=Constant Speed, 1=Fixed Pitch propeller_diameter= 6.0 //Propeller Diameter, (feet) propeller_blades= 3 //Number of propeller blades propeller_moi= 0.26 //Propeller moment of inertia beta_max= 0 //Maximum blade pitch angle for constant speed prop, (degrees) beta_min= 0 //Minimum blade pitch angle for constant speed prop, (degrees) min_gov_rpm= 0 //Miminum governed RPM prop_tc= 0.1 //Prop time-constant gear_reduction_ratio= 1.0 //Propeller gear reduction ratio fixed_pitch_beta= 13.75 //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 in feather 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] max_battery_voltage = 0 generator_alternator_voltage = 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 = 1.000, -10.713, 0.000, -2.54, 1500.000, 0, 0.25, 30.0, 0.15, 2.5, 0.85, 0.0, 0.0, 0.0, 0.0, 0.0 point.1 = 1.000, 0.716, -2.781, -3.60, 1500.000, 1, 0.85, 0.00, 0.15, 2.5, 0.85, 0.0, 0.0, 2.0, 0.0, 0.0 point.2 = 1.000, 0.716, 2.781, -3.60, 1500.000, 2, 0.85, 0.00, 0.15, 2.5, 0.85, 0.0, 0.0, 3.0, 0.0, 0.0 max_number_of_points = 21 static_pitch= 3.020 static_cg_height= 3.765 [Views] eyepoint=-2.057, 0.0, 0.991 //(feet) longitudinal, lateral, vertical distance from reference datum [exits] number_of_exits = 1 exit_rate.0 = 0.4 ;Percent per second [Radios] // Radio Type = availiable, standby frequency, has glide slope Audio.1 = 0 Com.1 = 1, 0 Nav.1 = 0, 0, 0 Adf.1 = 0 Transponder.1 = 0 Marker.1 = 0 [LIGHTS] //Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit //light.0=7, -2.4 ,0.00, 0.121, fx_rotax_fail [EFFECTS] wake=fx_spray water=fx_spray dirt=fx_none concrete=fx_none touchdown=fx_none startup=fx_engstrt [SMOKESYSTEM] smoke.0=13.0,3.0,0.0, fx_flour2q.fx [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, 3000 [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 [fuel] Center1=-1.485,0.000000,-2.543,22.000000,0.000000 fuel_type=1.000000 number_of_tank_selectors=1 electric_pump=1 [airplane_geometry] wing_area=152.000000 wing_span=30.00 wing_root_chord=4.916670 wing_dihedral=3.0 //Degrees wing_incidence=-1.0 //Degrees wing_twist=1.0 //Degrees oswald_efficiency_factor=0.9 //Measure of lift effeciency of wing wing_winglets_flag=0 wing_sweep=0.000000 wing_pos_apex_lon=-2.371000 wing_pos_apex_vert=0.000000 htail_area=39.000000 htail_span=11.666667 htail_pos_lon=-18.266667 htail_pos_vert=0.000000 htail_incidence=3.246460 htail_sweep=0.000000 vtail_area=15.8 //Square feet vtail_span=1.8 //Feet, tip to body vtail_pos_vert=-16.00000 elevator_area=16.610000 aileron_area=18.300000 rudder_area=23.20000 elevator_up_limit=28.000447 elevator_down_limit=20.998903 aileron_up_limit=19.996227 aileron_down_limit=15.000035 rudder_limit=33.995472 elevator_trim_limit=19.497754 spoiler_limit=45.000000 vtail_span=4.837355 vtail_sweep=0.000000 spoilerons_available=0 aileron_to_spoileron_gain=0.000000 min_ailerons_for_spoilerons=0.000000 min_flaps_for_spoilerons=0.000000 P_factor_scaler=0.1 vtail_pos_lon=-12.183333 [Reference Speeds] flaps_up_stall_speed=35.0 cruise_speed=48.0 never_exceed_speed=80.0 full_flaps_stall_speed=28.000000 max_indicated_speed=80.000000 [GeneralEngineData] engine_type=0 Engine.0=-1.400000,0.000000,0.000000 fuel_flow_scalar=1.36000 min_throttle_limit=0.000000 [autopilot] autopilot_available=0 flight_director_available=0 default_vertical_speed=700.000000 autothrottle_available=0 pitch_takeoff_ga=8.000000 autoland_available=0 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 [hydraulic_system] normal_pressure=0.000000 [stall_warning] type=1 [attitude_indicators] attitude_indicator.0=1 [turn_indicators] turn_indicator.0=1,0 [brakes] parking_brake = 1 //Parking brake available toe_brakes_scale = 1 //Brake scalar [Flaps.0] type=0 span-outboard=0.000000 extending-time=0.000000 system_type=0
