[fltsim.0] title=X-Wing sim=xwing model= panel= sound= texture= checklists= atc_id=N837KV atc_airline=USAF ui_manufacturer=Fictional ui_type=X-Wing fighter ui_variation=Red 5 description=Incom Corporations T-65 X-Wing Starfighter\n Shortly before the Emperor seized total control, the designers at Incom, disgusted with Incom's growing Imperial loyalty, stole the plans and working prototypes of the X-wing and defected to the Alliance. The X-wing's actual name is the T-65 Space Superiority Fighter, but the Rebels, following the tradition begun by the Y-wing fighter, dubbed it the "X-wing" due to its distinctive S-Foil positioning. The S-Foils, normally closed during hyperspace or atmospheric flight, open into an "X" during combat. This positioning increases the target range of the ship's lasers. The X-wing is probably the Alliance's best, most reliable starfighter. Its shields and hull are sturdy enough to withstand several hits, and its four laser cannons and two proton torpedo launchers give it ample firepower to deal with enemy fighters and capital ships alike. The inclusion of an astromech droid makes onboard repairs possible, even during battle. visual_damage=1 [General] performance=POWER SYSTEM: Novaldex O4-Z cryogenic power cells and Ionization reactor\nPROPULSION SYSTEM: Four Incom 4j.4 fusial thrust engines (rated at 300KTU)\nFLIGHT CONTROL SYSTEM: Torplex Rq8.Y flight control avionics package\nMANUEVERABILITY RATING: 75 DPF\nNAVIGATION: One astromech droid (usually an R2 unit) (Carried in a patch-in cradle behind the cockpit)\nHYPERDRIVE: Incom Gbk-585 motivator drive unit\nSENSOR SYSTEMS: Fabritech ANS-5d unit with LR Phased Tachyon Detection Array (PA-9r) SR Primary Threat Analysis Grid (PG-7u)\nTARGETING COMPUTER: Fabritech ANq 3.6 tracking computer with IN-344-B "Sightline" holographic imaging system\nWEAPONS: Four Taim & Bak IX4 laser cannons (single fire or fire-linked) Two Krupx MG7 proton torpedo launchers (three torpedos each)\nDEFENSE: Forward / rear projecting Chempat shields (rated at 50 SBD) Titanium alloy hull (rated at 20 RU) [WEIGHT_AND_BALANCE] // reference_datum_position=0.000000,0.000000,7.500000 reference_datum_position=0.0,0.0,0.0 empty_weight_CG_position=0.000000,0.000000,3.000000 max_number_of_stations=50 station_load.0=0.000000,0.000000,0.000000,0.000000 // empty_weight=39000.000000 // max_gross_weight= 43958.000 empty_weight=49000.000000 max_gross_weight= 53958.000 // Moments of Inertia (stability at speed) empty_weight_roll_MOI=1500000.0 empty_weight_pitch_MOI=1850000.0 empty_weight_yaw_MOI=1300000.0 empty_weight_coupled_MOI=1300.0 [fuel] LeftMain=0.000000,0.000000,0.000000,370.000000,0.000000 RightMain=0.000000,0.000000,0.000000,370.000000,0.000000 fuel_type=2.000000 number_of_tank_selectors=1 [airplane_geometry] wing_area=941.0 wing_span=47.50 wing_root_chord=7.3 wing_dihedral=2.5 wing_incidence=0.5 wing_twist=-1.5 oswald_efficiency_factor=75.0 // alters the ceiling + for higher wing_winglets_flag=0 wing_sweep=35.000000 wing_pos_apex_lon=0.0 wing_pos_apex_vert=0.000000 htail_area=42.000000 htail_span=41.666667 htail_pos_lon=-40.833333 htail_pos_vert=0.000000 htail_incidence=0.000000 htail_sweep=25.000000 vtail_area=45.000000 vtail_span=24.186773 vtail_sweep=30.000000 vtail_pos_lon=-37.500000 vtail_pos_vert=5.833333 elevator_area=100.000000 aileron_area=37.640000 rudder_area=76.500000 elevator_up_limit=27.501974 elevator_down_limit=20.626481 aileron_up_limit=19.480565 aileron_down_limit=14.896903 rudder_limit=23.491270 elevator_trim_limit=19.480565 spoiler_limit=59.988681 spoilerons_available=0 aileron_to_spoileron_gain=0.000000 min_ailerons_for_spoilerons=0.000000 min_flaps_for_spoilerons=0.000000 [contact_points] //0 Class 0-none 1-wheel 2-scrape point 3-skid 4-float 5-water rudder //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 / Water Rudder Effectiveness (0=Undamped, 1=Critically Damped) / 1.0 = normal //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) point.0=1.0 ,17.2, 0.0, -6.0, 1574.8, 0.0, 0.6475, 43.1, 0.25, 2.5, 0.7, 2.0, 2.0, 0.0, 0.0, 0.0 point.1=1.0 ,-9.5, -6.0, -6.0, 1574.8, 1.0, 0.6475, 0.0, 0.25, 2.5, 0.7, 2.0, 2.0, 2.0, 0.0, 0.0 point.2=1.0 ,-9.5, 6.0, -6.0, 1574.8, 2.0, 0.6475, 0.0, 0.25, 2.5, 0.7, 2.0, 2.0, 3.0, 0.0, 0.0 point.3=2.0 ,-11.0, 18.0, 0.0, 1574.8, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 5.0, 0.0, 0.0 point.4=2.0 ,-11.0, -18.0, 0.0, 1574.8, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 6.0, 0.0, 0.0 point.5=2.0 ,-5.0, 0.0, 5.0, 1574.8, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 9.0, 0.0, 0.0 point.6=2.0 ,27.3, 0.0, -0.7, 1574.8, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 4.0, 0.0, 0.0 point.7=2.0 ,-17.0, 0.0, -3.0, 1574.8, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 4.0, 0.0, 0.0 // need this to enable water rudder //point.8= 5, -30.90, -5.250, -7.300, 1600, 0, 0.00, 50.0, 0.0, 0.0, 1.00, 1.0, 1.2, 0, 0.0, 0.0 //point.9= 5, -30.90, 5.250, -7.300, 1600, 0, 0.00, 50.0, 0.0, 0.0, 1.00, 1.1, 1.5, 0, 0.0, 0.0 static_pitch=0.000000 static_cg_height=5.4 // need this to enable wing folding // [folding_wings] // wing_fold_system_type=4 // fold_rates=0.5,0.5 ;Percent per second // need this to enable tailhook [TailHook] tailhook_length=4 ;(feet) tailhook_position=-8.0, 0.0, -6.0 ;(feet) longitudinal, lateral, vertical positions from datum cable_force_adjust=1.0 [flaps.0] type = 1 // 1 - tail edge , 2 - lead edge system_type = 0 // 0-Electrical, 1-Hydraulic, 2-Pneumatic or 3-Manual span-outboard = 0.8 // 0.0 .. 1.0 extending-time = 0.5 // seconds lift_scalar = 1.0 // increase or decrease the amount of lift generated by flap deployment // drag_scalar = 1.4 // increase or decrease the amount of drag generated by flap drag_scalar = 1.0 // increase or decrease the amount of drag generated by flap // +pitch down, -pitch up pitch_scalar = -60.0 // adjust the tendency of the aircraft to pitch with flap deployment // flaps-position.0 = 0 // degrees // flaps-position.1 = 8 // degrees // flaps-position.2 = 16 // degrees // flaps-position.3 = 32 // degrees flaps-position.0 = 0 // degrees flaps-position.1 = 2 // degrees flaps-position.2 = 6 // degrees flaps-position.3 = 15 // degrees damaging-speed = 450 // KIAS blowout-speed = 700 // KIAS [GeneralEngineData] engine_type=1 //0=Piston, 1=Jet, 2=None, 3=Helo-Turbine, 4=Rocket, 5=Turboprop Engine.0=-6.0,6.0,4.0 //(feet) longitudinal, lateral, vertical distance from reference datum Engine.1=-6.0,-6.0,4.0 Engine.2=-6.0,6.0,-4.0 //(feet) longitudinal, lateral, vertical distance from reference datum Engine.3=-6.0,-6.0,-4.0 fuel_flow_scalar=0.1 [SMOKESYSTEM] smoke.0=-6.00, 5.00, 6.00, fx_smoke_rx smoke.1=-6.00, -5.00, 6.00, fx_smoke_rx smoke.2=-6.00, 5.00, -6.00, fx_smoke_rx smoke.3=-6.00, -5.00, -6.00, fx_smoke_rx [TurbineEngineData] fuel_flow_gain=0.002170 inlet_area=48.119880 rated_N2_rpm=29920.000000 // static_thrust=35099.900000 static_thrust=33500.0 afterburner_available=0 reverser_available=1 [Reference Speeds] flaps_up_stall_speed=5.0 full_flaps_stall_speed=4.0 cruise_speed=834.472682 [keyboard_response] elevator=150.000000,250.000000 aileron=150.000000,250.000000 rudder=150.000000,250.000000 [Views] eyepoint=3.3,0.0,3.291 // +Fore\-Aft,+Right\-Left,+Up\-Down [autopilot] autopilot_available=1 flight_director_available=0 default_vertical_speed=1800.000000 autothrottle_available=1 autothrottle_arming_required=0 autothrottle_takeoff_ga=0 autothrottle_max_rpm=90.000000 pitch_takeoff_ga=8.000000 [direction_indicators] direction_indicator.0=3,0 [EFFECTS] wake=fx_wake water=fx_spray dirt=fx_tchdrt concrete=fx_sparks touchdown=fx_tchdwn_s, 1 [LIGHTS] // Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing // +Fore\-Aft,+Right\-Left,+Up\-Down // light.0 = 2, -11.0, -25.3, 4.0, fx_strobeh , // light.1 = 2, -11.0, 25.3, 4.0, fx_strobeh , // light.2 = 1, 8.0, 0.0, 6.8, fx_beaconh , light.0 = 4, 3.3, 0, 3.291, fx_vclighth, [flight_tuning] cruise_lift_scalar = 1.0 parasite_drag_scalar = 0.3 induced_drag_scalar = 0.3 elevator_effectiveness = 0.7 aileron_effectiveness = 0.85 rudder_effectiveness = 0.35 pitch_stability = 1.0 roll_stability = 1.0 yaw_stability = 2.0 elevator_trim_effectiveness = 1.0 aileron_trim_effectiveness = 1.0 rudder_trim_effectiveness = 1.0
