[fltsim.0] title=Sportster sim=Sportster model= panel= sound= texture= kb_checklists= ui_manufacturer=Robbins Motors ui_type=Harley Davidson Sportster ui_variation=Custom Blue atc_heavy=0 atc_airline= description="The famous Harley Sportster Motorcycle, vintage 2006. Custom Blue." [fltsim.1] title=Sportster Paint1 sim=Sportster model= panel=1 sound= texture=1 kb_checklists= ui_manufacturer=Robbins Motors ui_type=Harley Davidson Sportster ui_variation=Custom Copper atc_heavy=0 atc_airline= description="The famous Harley Sportster Motorcycle, vintage 2006. Custom Copper." [fltsim.2] title=Sportster Paint2 sim=Sportster model= panel=2 sound= texture=2 kb_checklists= ui_manufacturer=Robbins Motors ui_type=Harley Davidson Sportster ui_variation=Factory Black/white trim atc_heavy=0 atc_airline= description="The famous Harley Sportster Motorcycle, vintage 2006. Factory Black." [fltsim.3] title=Sportster Paint3 sim=Sportster model= panel=3 sound= texture=3 kb_checklists= ui_manufacturer=Robbins Motors ui_type=Harley Davidson Sportster ui_variation=Custom Yellow atc_heavy=0 atc_airline= description="The famous Harley Sportster Motorcycle, vintage 2006. Custom Yellow." [General] atc_type= atc_model= editable=1 performance=Maximum Speed\t110 mph [Reference Speeds] flaps_up_stall_speed = 0 full_flaps_stall_speed = 0 cruise_speed = 055 max_indicated_speed = 115kts max_mach = 0.50 [WEIGHT_AND_BALANCE] max_gross_weight = 11500 empty_weight = 10500 reference_datum_position = 0.0000, 0.0000, 0.0000 // (feet) distance from FlightSim Reference position: (1/4 chord, centerline, waterline) empty_weight_CG_position = 0,0,1.5 ;ZXY distance from specified datum max_number_of_stations = 30 station_load.0 = 40, 0,0,0 ;Fuel station_load.1 = 350, 0,0,0 ;Driver station_load.3 = 500, -5,0,0; Passenger Luggage, misc. ;Moments of Inertia empty_weight_pitch_MOI = 74110 empty_weight_roll_MOI = 142310 empty_weight_yaw_MOI = 149000 empty_weight_coupled_MOI = 0 [contact_points] ; 0 Class (0=floats) ; 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=rigid) ; 9 Max/Static Compression Ratio ;10 Damping Ratio/Water Rudder Effectiveness (0=Undamped, 1=Critically Damped) ;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) ; 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=1, 7,-3, -2.5, 99999, 1, 1.5, 40, 1, 23.5, 1.65, 00, 00, 2, 60, 100 point.1=1, 7, 3, -2.5, 99999, 1, 1.5, 40, 1, 23.5, 1.65, 00, 00, 3, 60, 100 point.2=1, -8, -3,-2.5, 99999, 2, 1.5, 40, 1, 23.5, 1.65, 00, 00, 2, 60, 100 point.3=1, -8, 3, -2.5, 99999, 2, 1.5, 40, 1, 23.5, 1.65, 00, 00, 3, 60, 100 point.4=4, 7,-3, -2.5, 99999, 1, 1.5, 40, 1, 23.5, 1.65, 00, 00, 2, 60, 100 point.5=4, 7, 3, -2.5, 99999, 1, 1.5, 40, 1, 23.5, 1.65, 00, 00, 3, 60, 100 point.6=4, -8, -3,-2.5, 99999, 2, 1.5, 40, 1, 23.5, 1.65, 00, 00, 2, 60, 100 point.7=4, -8, 3, -2.5, 99999, 2, 1.5, 40, 1, 23.5, 1.65, 00, 00, 3, 60, 100 static_pitch = 0.1000 //degrees (pitch when loaded on ground) static_cg_height= 1 //feet, altitude of CG when at rest on the ground gear_system_type = 0 [Views] ;ZXY distance from reference datum (feet) eyepoint= -2.5, 0, 4 //(feet) longitudinal, lateral, vertical distance from reference datum [EFFECTS] wake=fx_wake water=fx_spray dirt=no_dirt concrete=no sparks touchdown=fx_tchdwn_s, 1 [flight_tuning] cruise_lift_scalar = .000 parasite_drag_scalar = 2.000 induced_drag_scalar = 2.000 elevator_effectiveness = .000 aileron_effectiveness = 000 rudder_effectiveness = 1 pitch_stability = 2.000 roll_stability = 1.000 yaw_stability =1.000 elevator_trim_effectiveness = .000 aileron_trim_effectiveness =.000 rudder_trim_effectiveness = 1.000 [airplane_geometry] wing_area = 125.0 ;Square feet wing_span = 111.4 wing_root_chord = 8.8 wing_dihedral = 7.0 ;Degrees wing_incidence = 2.0 ;Degrees wing_twist = -1.0 ;Degrees oswald_efficiency_factor = 0 ;Measure of lift effeciency of wing wing_winglets_flag = 0 ;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 = 470 ;Square feet htail_span = 7.8 htail_pos_lon = -10.0 ;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 = 0 ;Square feet aileron_area = 70 ;Square feet rudder_area = 200 ;Square feet elevator_up_limit = 0 ;Degrees elevator_down_limit = 0 ;Degrees aileron_up_limit = 0 ;Degrees aileron_down_limit = 0 ;Degrees rudder_limit = 25.5 ;Degrees elevator_trim_limit = 0 ;Degrees spoiler_limit = 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 = 0 [GeneralEngineData] engine_type = 1 ;1=Jet Engine.0 = -4,0,0 ;ZXY distance from ref datum fuel_flow_scalar = .0008 ;Scalar for fuel flow efficiency min_throttle_limit = 0 ;neg for turbine reverser [TurbineEngineData] fuel_flow_gain = 1.0 ;Gain on fuel flow inlet_area = 2.0 ;Square Feet, engine nacelle inlet area rated_N2_rpm = 9920 ;RPM, 2nd stage compressor rated value static_thrust = 58000 ;Lbs, max rated static thrust at SL afterburner_available = 0 ;Afterburner available? reverser_available = 0 ;Thrust reverser available? [jet_engine] thrust_scalar = 2.0 [fuel] Center1 = 0,0,0,7,0 ;ZXY GAL MIN fuel_type = 1 number_of_tank_selectors = 1 electric_pump = 1 [electrical] electric_always_available = 0 [Radios] // Radio Type = available, standby frequency, has glide slope Audio.1 = 1 Com.1 = 1, 0 Com.2 = 1, 0 Nav.1 = 1, 0, 1 Nav.2 = 1, 0, 1 Adf.1 = 1 Transponder.1 = 1 Marker.1 = 1 [gear_warning_system] gear_warning_available = 0 [brakes] parking_brake = 1 ;Parking brake available toe_brakes_scale = 2 ;Brake scalar [hydraulic_system] normal_pressure = 2000 ;PSI electric_pumps = 1 ;electric pumps engine_map = 1,0,0,0 ;pumps [pitot_static] vertical_speed_time_constant = 0 [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= 0 flight_director_available= 0 default_vertical_speed= 1000.0 autothrottle_available=0 autothrottle_arming_required=0 autothrottle_max_rpm = 0 autothrottle_takeoff_ga= pitch_takeoff_ga= max_pitch=12.0 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=0 max_bank_acceleration=2.8 max_bank_velocity=4.00 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] 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 [Flaps.0] type=0 span-outboard=0.000000 extending-time=0.000000 system_type=0
