[fltsim.0] title=Sith Fighter sim=sith_fighter model=sith_fighter [General] editable=0 [WEIGHT_AND_BALANCE] max_gross_weight=900000.000 empty_weight=0 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.0=0.0,0.0,0.0,0.0 ;Moments of Inertia empty_weight_roll_MOI=80000.000 empty_weight_pitch_MOI=145000.000 empty_weight_yaw_MOI=100000.000 empty_weight_coupled_MOI=1300.000 CG_forward_limit=0.000 CG_aft_limit=1.000 [fuel] LeftMain =0.000, 0.000, 0.000, 100.000, 0.000 LeftAux =0.000, 0.000, 0.000, 100.000, 0.000 RightMain=0.000, 0.000, 0.000, 100.000, 0.000 RightAux =0.000, 0.000, 0.000, 100.000, 0.000 fuel_type=2 number_of_tank_selectors=1 [airplane_geometry] wing_area=1002.000 wing_span=45.833 wing_root_chord=21.833 wing_dihedral=3.999 wing_incidence=-0.494 wing_twist=-1.000 oswald_efficiency_factor=3.501 wing_winglets_flag=0 wing_sweep=0.000 wing_pos_apex_lon=0.000 wing_pos_apex_vert=0.000 htail_area=200.000 htail_span=21.583 htail_pos_lon=-20.833 htail_pos_vert=0.000 htail_incidence=0.000 htail_sweep=0.000 vtail_area=350.000 vtail_span=21.331 vtail_sweep=0.000 vtail_pos_lon=-12.500 vtail_pos_vert=5.833 elevator_area=50.000 aileron_area=40.040 rudder_area=59.500 elevator_up_limit=9.5 elevator_down_limit=9.5 aileron_up_limit=9.5 aileron_down_limit=9.5 rudder_limit=20.0 elevator_trim_limit=19.0 spoiler_limit=180.0 spoilerons_available=0 aileron_to_spoileron_gain=0.000 min_ailerons_for_spoilerons=0.000 min_flaps_for_spoilerons=0.000 [contact_points] //For more detailed info read: Aircraft Container Overview.doc (Part of the CFS3 Aircraft and Vehicle SDK) //0 Class (0=None, 1=Wheel, 2=Scrape, 3=Skid, 4=Float, 5=Water Rudder) //1 Longitudinal Position (Distance of the point from the defined reference datum, in feet) //2 Lateral Position (Distance of the point from the defined reference datum, in feet) //3 Vertical Position (Distance of the point from the defined reference datum, in feet) //4 Impact Damage Threshold (The speed at which an impact with the ground can cause damage, in feet/min) //5 Brake Map (0=None, 1=Left, 2=Right) //6 Wheel Radius (Radius of the wheel, in feet) //7 Steer Angle (Maximum pivot angle in degrees) //8 Static Compression (Distance gear is compressed if aircraft is on the ground, in feet 0=rigid) //9 Max/Static Compression Ratio (Ratio of the maximum compression available to the static value) //10 Damping Ratio (0=Undamped, 1=Critically Damped) //11 Extension Time (Time it takes the gear to fully extend, in seconds 0=fixed gear) //12 Retraction Time (Time it takes the gear to fully retract, in seconds 0=fixed gear) //13 Sound Type (0-9 This will map a type of sound to a contact point) //14 Airspeed limit (This is the speed at which the gear extension will give a warning, in KIAS) //15 Damage from airspeed (The speed at which the extended gear gets damaged, in KIAS) // 0 1 2 3 4 5 6 7 8 9 10 11 12 13 14 15 point.0= 1, -15.5, 0.0, -9.97, 9999.9, 0, 0.1, 48, 0.400000, 2.5, 0.553761, 1.7, 1.7, 0, 0.0, 0.0 point.1= 1, 15.0, -13.0, -9.97, 9999.9, 1, 0.1, 0.0, 0.400000, 2.5, 0.553732, 1.7, 1.7, 2, 0.0, 0.0 point.2= 1, 15.0, 13.0, -9.97, 9999.9, 2, 0.1, 0.0, 0.400000, 2.5, 0.553732, 1.7, 1.7, 3, 0.0, 0.0 point.3= 2, 15.0, -13.0, -7.97, 9999.9, 0, 0.0, 0.0, 0.000000, 0.0, 0.000000, 0.0, 0.0, 4, 0.0, 0.0 point.4= 2, 15.0, 13.0, -7.97, 9999.9, 0, 0.0, 0.0, 0.000000, 0.0, 0.000000, 0.0, 0.0, 4, 0.0, 0.0 point.5= 2, 0.0, -13.0, -7.97, 9999.9, 0, 0.0, 0.0, 0.000000, 0.0, 0.000000, 0.0, 0.0, 5, 0.0, 0.0 point.6= 2, 0.0, 13.0, -7.97, 9999.9, 0, 0.0, 0.0, 0.000000, 0.0, 0.000000, 0.0, 0.0, 6, 0.0, 0.0 point.7= 2, -15.0, -13.0, -7.97, 9999.9, 0, 0.0, 0.0, 0.000000, 0.0, 0.000000, 0.0, 0.0, 9, 0.0, 0.0 point.8= 2, -15.0, 13.0, -7.97, 9999.9, 0, 0.0, 0.0, 0.000000, 0.0, 0.000000, 0.0, 0.0, 9, 0.0, 0.0 static_pitch=0.0 static_cg_height=9.97 [Flaps.0] type=1 span-outboard=0.500 extending-time=3.000 system_type=0 damaging-speed=0.000 blowout-speed=0.000 lift_scalar=1.000 drag_scalar=1.000 pitch_scalar=-1.000 flaps-position.0=0.000, 0.000 flaps-position.1=3.000, 0.000 flaps-position.2=9.000, 0.000 flaps-position.3=35.000, 0.000 flaps-position.4=85.000, 0.000 [Reference Speeds] flaps_up_stall_speed=10.000 full_flaps_stall_speed=5.000 cruise_speed=600.000 [GeneralEngineData] engine_type=1 Engine.0=0.000, 0.000, 0.000 engine.1=0.000, 0.000, 0.000 fuel_flow_scalar=0.100 [TurbineEngineData] fuel_flow_gain=0.002 inlet_area=31.861 rated_N2_rpm=29920.000 static_thrust=14000.0 afterburner_available=0 reverser_available=1 fuel_flow_scalar=0.100000 thrust_scalar=1.000000 [keyboard_response] elevator=150.000000,250.000000 aileron=150.000000,250.000000 rudder=150.000000,250.000000
