[fltsim.0] title=XP2V-1 (Vega 156 model) sim=XP2V model= panel= sound= texture= kb_checklists= [WEIGHT_AND_BALANCE] max_gross_weight=48000.000 empty_weight=29189.000 reference_datum_position=0.000, 0.000, 0.000 empty_weight_CG_position=0.000, 0.000, 0.000 max_number_of_stations=50 station_load.4=0, -12.67, -1.1, 0.0 //Passenger Weight (lbs), longitudinal, lateral, vertical positions from datum (feet) station_load.5=0, -12.67, 1.1, 0.0 //Passenger Weight (lbs), longitudinal, lateral, vertical positions from datum (feet) station_load.6=0, -15.00, 0.0, 0.0 //Baggage Weight (lbs), longitudinal, lateral, vertical positions from datum (feet) ;Moments of Inertia empty_weight_pitch_MOI=1000000.000 empty_weight_roll_MOI=500000.000 empty_weight_yaw_MOI=900000.000 empty_weight_coupled_MOI=0.000 CG_forward_limit=0.000 CG_aft_limit=1.000 station_load.0=0.000000,0.000000,0.000000,0.000000 [flight_tuning] cruise_lift_scalar=1.0 parasite_drag_scalar=1.0 induced_drag_scalar=1.0 elevator_effectiveness=1.0 aileron_effectiveness=1.0 rudder_effectiveness=1.0 pitch_stability=1.0 roll_stability=1.0 yaw_stability=1.0 elevator_trim_effectiveness=1.0 aileron_trim_effectiveness=1.0 rudder_trim_effectiveness=1.0 [piston_engine] power_scalar=1.0 [propeller] thrust_scalar=1.0 rotation= -1,1 //Engine 1,2,3,... Rotation direction. 1 = CW, -1 = CCW [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 (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) //GEAR point.0=1.000, 18.210, 0.000, -9.700, 1600.000, 0.000, 2.000, 60.000, 0.500, 0.500, 1.000, 8.000, 6.000, 0.000, 0.000, 0.000 point.1=1.000, -4.070, -12.960, -10.350, 1600.000, 1.000, 2.460, 0.000, 0.500, 2.500, 0.850, 8.000, 10.000, 2.000, 0.000, 0.000 point.2=1.000, -4.070, 12.960, -10.350, 1600.000, 2.000, 2.460, 0.000, 0.500, 2.500, 0.850, 8.000, 10.000, 3.000, 0.000, 0.000 //SCRAPES point.3=2.000, 0.760, -18.910, 0.500, 800.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 5.000, 0.000, 0.000 point.4=2.000, 0.760, 18.910, 0.500, 800.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 6.000, 0.000, 0.000 point.5=2.000, -17.080, 0.000, -0.500, 800.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 9.000, 0.000, 0.000 point.6=2.000, 7.360, 0.000, -1.240, 800.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 4.000, 0.000, 0.000 static_pitch=0.000 static_cg_height=10.350 [electrical] max_battery_voltage=24.0 generator_alternator_voltage=28.0 max_generator_alternator_amps=60.0 [exits] number_of_exits=1 exit_rate.0=0.4 ;Percent per second [Views] eyepoint=-8.213, -0.8612, 2.220 //Longitudinal, Lateral, Vertical (feet) [airplane_geometry] wing_area=1250.000 wing_span=108.000 wing_root_chord=15.000 wing_dihedral=2.000 wing_incidence=0.000 wing_twist=-1.000 oswald_efficiency_factor=0.750 wing_winglets_flag=0 wing_sweep=0.000 wing_pos_apex_lon=0.000 wing_pos_apex_vert=0.000 htail_area=272.000 htail_span=37.000 htail_pos_lon=-40.000 htail_pos_vert=3.500 htail_incidence=0.000 htail_sweep=5.000 vtail_area=156.000 vtail_span=12.000 vtail_sweep=35.000 vtail_pos_lon=-42.000 vtail_pos_vert=10.000 elevator_area=68.000 aileron_area=72.000 rudder_area=60.000 elevator_up_limit=17.000 elevator_down_limit=15.500 aileron_up_limit=18.000 aileron_down_limit=18.000 rudder_limit=30.000 elevator_trim_limit=5.000 spoiler_limit=0.000 spoilerons_available=0 aileron_to_spoileron_gain=0.000 min_ailerons_for_spoilerons=0.000 min_flaps_for_spoilerons=0.000 [Reference Speeds] flaps_up_stall_speed=120.000 full_flaps_stall_speed=90.000 cruise_speed=162.000 [forcefeedback] stick_shaker_magnitude=5000 ; 0 - 10000 stick_shaker_direction=0 ; 0 - 35999 degrees stick_shaker_period=111111 ; in microseconds 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=9000 ; 0 - 35999 degrees gear_bump_left_duration=250000 ; in microseconds gear_bump_right_magnitude=2700 ; 0 - 10000 gear_bump_right_direction=27000 ; 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=1 // 1 - tail, 2 - lead span-outboard=0.125 // 0.0 .. 1.0 extending-time=5 // seconds flaps-position.0=0 // degrees, KIAS flaps-position.1=25 // degrees, KIAS flaps-position.2=50 // degrees, KIAS damaging-speed=191 // KIAS blowout-speed=290 // KIAS
