// SAAB J35J Draken for FS2004 // Copyright (c) 2001-2006 Thomas Nilsson, Bookmark Digital Graphics // Version 2.4 // Aircraft.cfg last edited: 2006-03-20 [fltsim.0] title=SAAB 35XD Danish green paint scheme sim=j35bm_55 model= panel= sound= texture=AR-116 kb_checklists=35XD_check kb_reference=35XD_ref description=SAAB 35XD Draken for Flight Simulator 2004 \nVersion 2.41 2006-03-20 \n© 2006 Thomas Nilsson/Bookmark Digital Graphics\The Saab 35 Draken is a supersonic interceptor using a double delta wing. The first prototype of this aircraft flew late in 1955, entering production in 1957. The aircraft is a single-seat, single-engine configuration equipped with 30mm cannons and air-to-air Sidewinder missiles. It can operate from small airfields due to its high thrust-to-weight ratio and the fitment of a parachute to assist with braking. In all, over 600 Drakens were built, the last example taking to the air 1972. For Denmark the Saab 35XD was developed. Based on the J 35F but was upgraded with more internal fuel, stronger gear, arrester hook, improved avionics and cockpit layout, new weapon pylons which resulted in redesigned outer wings. Three versions were built from the Saab 35XD variant: Here a single seat fighter repainted in the liverie of "AR-116" Esk.729 by Claus Vendelboe Holmberg April 2006. ui_manufacturer=SAAB ui_type=35XD Draken ui_variation=RDAF AR-116 atc_parking_types=MIL_COMBAT atc_airline=Danish Air Force atc_id=AR-116 visual damage=0 [General] performance=Length: 15.4 m (50.5 ft) \nHeight: 3.89 m (12.8 ft) \nWing span: 9.4 m (30.8 ft) \nEmpty weight: 8250 kg (18188 lbs) \nMTOW: 12270 kg (27050 lbs) \nEngine: Volvo Flygmotor RM 6C (RR Avon Mk 300 big-bore) \nStatic thrust: 5845 kp, 7900 kp with reheater \nMax speed (clean): 2125 kph (1150 kts) \nService ceiling: 16000 m (52000 ft) \nRange (with stores): 1300 km (700 nm) \nArmament: \n 1 x 30mm Aden gun (in right wing) \n 2 x AIM-9B/J/L Sidewinders \n 2 x AIM-4F/26 Falcon AAMs \n Rocket pods \nCrew: Single seat atc_type=SAAB atc_model=35XD ///////////////////////////////////////////////////////////////////////////////////////// [WEIGHT_AND_BALANCE] reference_datum_position = 5.000, 0.000, 1.050 // 5.000,0.000,1.050 (feet) distance from reference position: (1/4 chord, centerline, waterline) empty_weight_CG_position = -2.500, 0.000, 0.000 // -2.5,0,0 (feet) long, lat, vert distance from specified datum max_number_of_stations=3 station_load.0 = 180.0, 7.000, 0.000, 0.000 // Pilot - Weight (lbs), longitudinal, lateral, vertical positions from datum (feet) station_load.1 = 400.0, 0.000, 0.000, 0.000 // Pylon 4 station_load.2 = 350.0, 0.000, 0.000, 0.000 // Pylon 7 max_gross_weight = 27000.000 //27000 empty_weight = 18200.000 //18200 empty_weight_roll_MOI = 75000.000 // 75000 empty_weight_pitch_MOI = 420000.000 //420000 empty_weight_yaw_MOI = 100000.000 //100000 empty_weight_coupled_MOI = 0.000 // 0 //CG_forward_limit= 0.000 //CG_aft_limit= 1.000 [airplane_geometry] //default values for J35J v2.3 wing_area = 250.000 //250 - really 527 sqf for J35 wing_span = 30.000 //30.000 - feet wing_root_chord = 9.000 //9.000 - feet, not realistic for delta wings wing_dihedral = 6.000 //6.000 - degrees? only affects vertical MAC offset? wing_incidence = 0.000 //0.000 - degrees, affects cruise pitch? wing_twist = 0.000 //0.000 - degrees, affects cruise pitch? oswald_efficiency_factor = 0.300 //0.250 - lift efficiency of wing (the J35 glides like a brick) wing_winglets_flag = 0 //0 - bool wing_sweep = 55.000 //55.000 - degrees, wing leading edge wing_pos_apex_lon = 11.000 //11.000 - feet, longitudinal distance from ref point, negative going aft wing_pos_apex_vert = 0.000 //0.000 - feet, vertical distance from ref point, positive going up htail_area = 0.000 //0.000, no effect htail_span = 0.000 //0.000, no effect htail_pos_lon = 0.000 //0.000, no effect htail_pos_vert = 0.000 //0.000, no effect htail_incidence = 0.000 //0.000 - 0.0 to 3.0 may improve pitch stability // Set Sign for DOWN force on tail. H. Stab CL ~-0.02 (~5% of CL wing in cruise [AFSD displays this]) htail_sweep = 0.000 //0.000, has no effect vtail_area = 50.000 //50.000 - no effect? vtail_span = 8.062 //8.062 - no effect? vtail_sweep = 0.000 //0.000 - no effect? vtail_pos_lon = -19.167 //-19.167 - no effect? vtail_pos_vert = 5.833 //5.833 - no effect? elevator_area = 0.000 //0.000 - no effect aileron_area = 0.000 //0.000 - no effect rudder_area = 0.000 //0.000 - no effect elevator_up_limit = 20.000 //18.000 elevator_down_limit = 12.000 //12.000 aileron_up_limit = 10.000 //10.000 aileron_down_limit = 10.000 //10.000 rudder_limit = 25.000 //25.000 elevator_trim_limit = 20.000 //20.000 spoiler_limit = 60.000 //60.000 spoilerons_available = 0 //0 aileron_to_spoileron_gain = 0.000 //0.000 min_ailerons_for_spoilerons = 0.000 //0.000 min_flaps_for_spoilerons = 0.000 //0.000 [Reference Speeds] flaps_up_stall_speed = 150.000 full_flaps_stall_speed = 150.000 cruise_speed = 450.000 max_indicated_speed = 1200.00 max_mach = 2.00 [flight_tuning] cruise_lift_scalar = 1.000 // 1.000 - affects cruise pitch, set higher to reduce aoa on final pitch_stability = 4.500 // 4.500 - very high to avoid oscillating, the real J35 has damping roll_stability = 1.900 // 2.000 yaw_stability = 2.000 // 2.000 parasite_drag_scalar = 1.500 // 1.500 induced_drag_scalar = 1.200 // 1.200 elevator_effectiveness = 3.800 // 3.800 - set very high to compensate for high pitch stability aileron_effectiveness = 6.800 // 6.000 - set very high to compensate for high roll stability rudder_effectiveness = 0.300 // 0.300 - usually set way too high in FS9 aircraft elevator_trim_effectiveness = 5.000 // 5.000 aileron_trim_effectiveness = 1.000 // 1.000 rudder_trim_effectiveness = 1.000 // 1.000 [GeneralEngineData] engine_type = 1 // 0=Piston, 1=Jet, 2=None, 3=Helo-Turbine, 4=Rocket, 5=Turboprop Engine.0 = -9.0, 0.0, 4.0 //-9.0, 0.0, 4.0 - long, lat, vert distance in feet from reference datum fuel_flow_scalar = 1.35 // 1.35 - affects fuel consumption min_throttle_limit = 0.0 // 0.0 - do NOT change this [TurbineEngineData] fuel_flow_gain = 0.0035 // 0.0035 - affects spool-up time inlet_area = 9.00 // 9.00 - affects RAM drag at high Mach rated_N2_rpm = 8050.00 // 8050 - set to nominal max rpm, 8370 = 104% static_thrust = 12900.00 // 12900 according to RM6C specs, 17400 with afterburner afterburner_available = 1 reverser_available = 0 [jet_engine] thrust_scalar = 1.45 // 1.55 - should be 1.0 if thrust curves correctly set... [brakes] parking_brake = 1 // boolean - parking brake available toe_brakes_scale = 0.8 // brake scalar - less than 1.0 is usually more realistic [flaps.0] // J35 has no flaps - this function is used for drag chute type = 1 // 1 = trailing edge, 2 = leading edge span-outboard = 1.0 // 0.0 ... 1.0 extending-time = 1.3 // seconds flaps-position.0 = 0 // degrees flaps-position.1 = 45 // degrees damaging-speed = 180 // KIAS blowout-speed = 200 // KIAS lift_scalar = 1.0 // 1.0 - not applicable drag_scalar = 1.5 // 1.0 - increase to improve chute braking pitch_scalar = 1.0 // 1.0 - not applicable system_type = 3 // 0=Electric, 1=Hydraulic, 2=Pneumatic, 3=Manual, 4=None //[TailHook] //tailhook_length=1 // (feet) //tailhook_position=-15.0, 0.0, -1.0 // (feet) longitudinal, lateral, vertical positions from datum //cable_force_adjust=1.0 //[folding_wings] //wing_fold_system_type=1 // 0=None //fold_rates=1.000,1.000 // Percent per second ///////////////////////////////////////////////////////////////////////////////////////// [hydraulic_system] normal_pressure = 3046.0 // psi electric_pumps = 1 // no. of electric pumps engine_map = 1,0,0,0 // pump on Eng1 [electrical] max_battery_voltage = 24.0 generator_alternator_voltage = 29.0 max_generator_alternator_amps = 40.0 engine_generator_map = 1,0,0,0 // Consumer = BusType, MaxAmpLoad, MinVoltage // BusTypes: 0=MainBus, 1=AvionicsBus, 2=BatteryBus, 3=HotBatteryBus, 4-7=Generator/AlternatorBus(1-4) // Bus Amps MinV flap_motor = 3, 0 20.0 gear_motor = 3, 0, 20.0 pitot_heat = 3, 1, 20.0 fuel_pump = 3, 1, 20.0 starter1 = 3, 12, 18.0 marker_beacon = 1, 1, 12.0 standby_vacuum = 3, 1, 12.0 light_nav = 3, 1, 12.0 light_recognition = 3, 1, 12.0 light_strobe = 3, 1, 12.0 light_panel = 3, 1, 12.0 light_cabin = 3, 1, 1.0 light_landing = 3, 1, 12.0 light_taxi = 3, 1, 12.0 autopilot = 3, 1, 20.0 avionics_bus = 3, 1, 20.0 avionics = 1, 1, 20.0 additional_system = 3, 1, 20.0 directional_gyro = 3, 1, 20.0 directional_gyro_slaving = 3, 1, 20.0 fuel_transfer_pump = 3, 1, 20.0 hydraulic_pump = 3, 1, 20.0 [fuel] fuel_type = 2 // 1=Avgas 2=JetA number_of_tank_selectors = 1 // max one for each engine electric_pump = 1 // boolean // Tank pos long lat vert usable unusable volume (USgal) Center1 = -2.000, 0.000, -0.000, 383.000, 0.000 // Forward tank group Center2 = 2.000, 0.000, -0.000, 383.000, 0.000 // Rear tank group External1 = 0.000, -1.667, -0.833, 138.000, 0.000 // Left drop tank External2 = 0.000, 1.667, -0.833, 138.000, 0.000 // Right drop tank [contact_points] max_number_of_points = 9 static_pitch= 4.500 static_cg_height= 5.8 gear_system_type=0 // 0=Electric, 1=Hydraulic, 2=Pneumatic, 3=Manual, 4=None //0 Class (0=none,1=wheel, 2=scrape, 3=skid, 4=float, 5=water rudder) //1 Longitudinal Position (feet) //2 Lateral Position (feet) //3 Vertical Position (feet, increase to raise from ground) //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 (calculated) //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 0 1 2 3 4 5 6 7 8 9 10 11 12 13 14 15 point.0= 1, -19.000, 0.000, -4.200, 2500.000, 0.000, 0.450, 0.000, 0.250, 2.500, 0.668, 5.000, 5.000, 0.000, 0.000, 300.000 //Spur Wheel point.1= 1, 7.000, 0.000, -7.020, 1500.000, 0.000, 0.950, 42.000, 0.250, 2.500, 0.668, 5.000, 5.000, 0.000, 0.000, 300.000 //Nose Gear point.2= 1, -6.500, -4.400, -6.270, 2200.000, 1.000, 1.220, 0.000, 0.300, 2.500, 0.850, 5.000, 5.000, 3.000, 0.000, 300.000 //L Main Gear 750 point.3= 1, -6.500, 4.400, -6.270, 2200.000, 2.000, 1.220, 0.000, 0.300, 2.500, 0.850, 5.000, 5.000, 3.000, 0.000, 300.000 //R Main Gear point.4= 2, -18.000, -15.000, -1.100, 0000.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 5.000, 0.000, 0.000 //L Wing point.5= 2, -18.000, 15.000, -1.100, 0000.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 6.000, 0.000, 0.000 //R Wing point.6= 2, 22.000, 0.000, -2.200, 0000.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 4.000, 0.000, 0.000 //Nose point.7= 2, -22.500, 0.000, 7.900, 0000.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 9.000, 0.000, 0.000 //Tail Fin point.8= 2, -25.500, 0.000, -1.200, 0000.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 9.000, 0.000, 0.000 //Tail End //point.9= 5, 0.000, 0.000, 0.000, 1500.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 1.000, 0.050, 0.000, 0.000, 0.000 //WR ////////////////////////////////////////////////////////////////////////////////////////////// [LIGHTS] //Types: 1=beacon, 2=strobe, 3=nav, 4=cockpit, 5=landing, 6=taxi, 7=recog, 8=wing, 9=logo, 10=cabin //---------------------------------------------------- // type Z X Y filename Z=longitudinal X=lateral Y=vertical //---------------------------------------------------- light.1= 3, -5.35, 0.00, -1.0, fx_j35_nav_dim, //lo-intensity navlights light.2= 7, -5.35, 0.00, -1.0, fx_j35_nav_brt, //hi-intensity navlights light.3= 2, -5.35, 0.00, -1.0, fx_j35_nav_flash, //flashing navlights light.4= 3, -20.80, 0.00, -0.9, fx_j35_tail_dim, //lo-intensity tail lights light.5= 7, -20.80, 0.00, -0.9, fx_j35_tail_brt, //hi-intensity tail lights light.6= 2, -20.80, 0.00, -0.9, fx_j35_tail_flash, //flashing tail lights //----------- wing vortex effects -------------------- light.7= 8, -18.0, -15.00, -1.0, fx_j35_wing_vtx, light.8= 8, -18.0, 15.00, -1.0, fx_j35_wing_vtx, [EFFECTS] wake= fx_wake water= fx_spray dirt= fx_tchdrt concrete= fx_sparks touchdown= fx_tchdwn, 1 contrail= fx_j35_contrail //adds contrail below -30c [SMOKESYSTEM] // (controlled by afterburner gauge) // Y Z X filename //---------------------------------------------------- smoke.0= 0.0, -28.00, 0.00, fx_j35_absmoke //vertical offset has no effect smoke.1= 0.0, -27.00, 0.00, fx_j35_abflame ////////////////////////////////////////////////////////////////////////////////////////////// [gear_warning_system] gear_warning_available=0 pct_throttle_limit=0.000000 flap_limit_power=0.000000 flap_limit_idle=0.000000 [stall_warning] type=0 [Radios] // avail, stby freq, 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 = 0 Transponder.1 = 1 Marker.1 = 1 [airspeed_indicators] // adjusts IAS vs TAS airspeed_indicator.0 = 0.8791, -1.7 // The first value is equivalent to the "Weighting Factor" scaled integer in REC 1101 // The second value is the IAS "Base Offset" [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 direction_indicator.1 = 1,0 direction_indicator.2 = 1,0 [attitude_indicators] //Type: 0=None, 1=Vacuum Gyro, 2=Electric Gyro attitude_indicator.0 = 1 attitude_indicator.1 = 1 [turn_indicators] //Type: 0=None, 1=Electric Gyro, 2= Vacuum Gyro turn_indicator.0 = 1,1 // TURN and BANK [exits] number_of_exits = 1 exit_rate.0 = 0.4 [keyboard_response] elevator = 150.000000,250.000000 aileron = 150.000000,250.000000 rudder = 150.000000,250.000000 [autopilot] autopilot_available = 1 flight_director_available = 1 default_vertical_speed = 800 // fpm default_pitch_mode = 0 default_bank_mode = 0 //use_no_default_pitch = 1 //use_no_default_bank = 1 autothrottle_available = 0 autothrottle_arming_required = 0 autothrottle_takeoff_ga = 0 autothrottle_max_rpm = 90.00 pitch_takeoff_ga = 8.00 // default TOGA pitch max_pitch = 10.00 // 10.0 max_pitch_acceleration = 1.00 // 1.0 max_pitch_velocity_lo_alt = 0.80 // 2.0 max_pitch_velocity_hi_alt = 0.30 // 1.5 max_pitch_velocity_lo_alt_breakpoint = 10000 // 20000 max_pitch_velocity_hi_alt_breakpoint = 40000 // 28000 max_bank = 30.00 // 30.0 max_bank_acceleration = 1.80 // 1.8 max_bank_velocity = 3.00 // 3.0 max_throttle_rate = 0.10 // 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 = 1.00 [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 [Views] eyepoint=6.05, 0.00, -1.28 // VC viewpoint Long/Lateral/Vert (J35 def: 6.05, 0.00, -1.40)
