----------------------------------F-16 VIPER (By KIRK OLSSON) ---------------------------------- [fltsim.0] title=F-16B OCU FB-17 sim=f16ocu model= panel= sound= texture= checklists= description=F-16B Fighting Falcon, Belgian Air Force \nKleine Brogel Air Base\nRepaint by Mathy "Math" Maesen ui_manufacturer=Lockheed Martin ui_type=F-16B OCU ui_variation= atc_heavy=0 atc_id=17 atc_airline=Air Force atc_flight_number=FB17 atc_type=LOCKHEED atc_model=F16 -------------------------------------------------------------------------------------- [General] performance= maximum level speed Mach 2.0 at 12190 m (40,000ft) > service ceiling above 15240 m (50,000 feet) > operational radius 925 km (575 miles) > empty 7070 kg (15,586 lb) > maximum take-off 16,057 kg (35,400 lb) -------------------------------------------------------------------------------------- [WEIGHT_AND_BALANCE] reference_datum_position= 0.000, 0.000, 0.000 empty_weight_CG_position= 0.000, 0.000, 0.000 max_number_of_stations=12 station_load.0 = "0.0, 0.0, 15.0, -0.3, left wingtip" //Weight (lbs), longitudinal, lateral, vertical positions from datum (feet) station_load.1 = "0.0, 0.0, 13.0, -0.5, left pylon 1" //Weight (lbs), longitudinal, lateral, vertical positions from datum (feet) station_load.2 = "0.0, 0.5, 11.0, -0.5, left pylon2" //Weight (lbs), longitudinal, lateral, vertical positions from datum (feet) station_load.3 = "0.0, 0.5, 9.0, -1.0, left pylon3" //Weight (lbs), longitudinal, lateral, vertical positions from datum (feet) station_load.4 = "00.0, 5.0, 1.0, -1.5, left lantirn pylon " //Weight (lbs), longitudinal, lateral, vertical positions from datum (feet) station_load.5 = "00.0, 3.0, 0.0, -2.5, center pylon " //Weight (lbs), longitudinal, lateral, vertical positions from datum (feet) station_load.6 = "00.0, 5.0, -1.0, -1.5, right lantirn pylon " //Weight (lbs), longitudinal, lateral, vertical positions from datum (feet) station_load.7 = "0.0, 0.5, -9.0, -1.0, right pylon 4" //Weight (lbs), longitudinal, lateral, vertical positions from datum (feet) station_load.8 = "0.0, 0.5, -11.0, -0.5, right pylon 5" //Weight (lbs), longitudinal, lateral, vertical positions from datum (feet) station_load.9 = "0.0, 0.0, -13.0, -0.5, right pylon 6" //Weight (lbs), longitudinal, lateral, vertical positions from datum (feet) station_load.10 = "0.0, 0.0, -15.0, -0.3, right wingtip" //Weight (lbs), longitudinal, lateral, vertical positions from datum (feet) station_load.11 = "200.0, 8.5, 0.0, 2.0, pilot" //Weight (lbs), longitudinal, lateral, vertical positions from datum (feet) empty_weight= 11000.000 empty_weight_roll_MOI= 40000.000 empty_weight_pitch_MOI= 48000.000 empty_weight_yaw_MOI= 24000.000 empty_weight_coupled_MOI= 4000.000 max_gross_weight= 32211.000 CG_forward_limit= 0.000 CG_aft_limit= 1.000 ---------------------------------------------------------------------------------------------------- [fuel] Center1= 0.000, 0.000, 0.000, 300.000, 0.000 LeftMain= 0.000, 0.000, 0.000, 525.000, 0.000 LeftAux= 0.000, -5.000, 0.000, 370.000, 0.000 LeftTip= 0.000, -10.000, 0.000, 0.000, 0.000 RightMain= 0.000, 0.000, 0.000, 525.000, 0.000 RightAux= 0.000, 5.000, 0.000, 370.000, 0.000 RightTip= 0.000, 10.000, 0.000, 0.000, 0.000 fuel_type=2.000000 number_of_tank_selectors=3 electric_pump=0 -------------------------------------------------------------------------------------------------------------- [airplane_geometry] wing_area= 245.000 wing_span= 30.500 wing_root_chord= 7.333 wing_dihedral= 0.000 wing_incidence= -0.494 wing_twist= -1.000 oswald_efficiency_factor= 1.071 wing_winglets_flag= 0 wing_sweep= 0.000 wing_pos_apex_lon= 0.000 wing_pos_apex_vert= 0.000 htail_area= 47.000 htail_span= 14.167 htail_pos_lon= -16.333 htail_pos_vert= 0.000 htail_incidence= 0.000 htail_sweep= 0.000 vtail_area= 40.000 vtail_span= 7.211 vtail_sweep= 0.000 vtail_pos_lon= -16.333 vtail_pos_vert= 5.833 elevator_area= 10.000 aileron_area= 6.880 rudder_area= 3.400 elevator_up_limit= 21.064 elevator_down_limit= 15.772 aileron_up_limit= 9.762 aileron_down_limit= 9.762 rudder_limit= 35.918 elevator_trim_limit= 19.481 spoiler_limit= 59.989 spoilerons_available= 0 aileron_to_spoileron_gain= 0.000 min_ailerons_for_spoilerons= 0.000 min_flaps_for_spoilerons= 0.000 ----------------------------------------------------------------------------------------------------------------------- [contact_points] 1 2 3 4 5 6 7 8 9 10 11 12 13 14 15 16 point.0= 1.000, 10.583, 0.000, -6.457, 1574.803, 0.000, 0.578, 37.620, 0.200, 1.700, 1.0, 6.300, 6.200, 0.000, 400.000, 0.000 point.1= 1.000, -2.500, -4.167, -6.687, 1574.803, 1.000, 0.578, 0.000, 0.605, 1.200, 1.2, 5.5, 5.600, 2.000, 400.000, 0.000 point.2= 1.000, -2.500, 4.167, -6.687, 1574.803, 2.000, 0.578, 0.000, 0.605, 1.200, 1.2, 5.5, 5.600, 3.000, 400.000, 0.000 point.3= 2.000, -6.417, -16.333, -0.167, 1574.803, 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, -6.417, 16.333, -0.167, 1574.803, 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, -19.750, 0.000, -1.833, 1574.803, 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, 22.667, 0.000, -1.250, 1574.803, 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= 6.265 gear_system_type=0 -------------------------------------------------------------------------------------------------------- [jet_engine] thrust_scalar=1.0 ------------------------------------------------------------------------------------------------------- [GeneralEngineData] engine_type= 1 Engine.0= -6.667, 0.000, 0.000 fuel_flow_scalar= 1.000 min_throttle_limit=0.000000 ------------------------------------------------------------------------------------------------------- [TurbineEngineData] fuel_flow_gain= 0.002 inlet_area= 3.617 rated_N2_rpm= 29920.000 static_thrust= 12300.000 afterburner_available= 1 reverser_available= 0 ------------------------------------------------------------------------------------------------------- [Reference Speeds] flaps_up_stall_speed= 79.000 full_flaps_stall_speed= 63.200 cruise_speed= 622.662 max_indicated_speed=1400.000000 max_mach=2.000000 ------------------------------------------------------------------------------------------------------ [keyboard_response] elevator=150.000000,250.000000 aileron=150.000000,250.000000 rudder=150.000000,250.000000 ------------------------------------------------------------------------------------------------------- [Views] eyepoint=15.1,-0.020000,3.68 VIEW_FORWARD_ZOOM=0.50 ---------------------------------------------------------------------------------------------------------- [exits] number_of_exits=1 exit_rate.0=0.2 ;Percent per second ---------------------------------------------------------------------------------------------------------------- [EFFECTS] wake=fx_wake water=fx_spray dirt=fx_tchdrt concrete=fx_sparks touchdown=fx_ktchdwn, 1 contrail=fx_F16ko_Contrail //adds contrail when temp is -30c //startup=fx_F16ko_JetStartHeat3 //smoke puff at startup, w/3 minutes of "heat" startup=fx_F16ko_JetStartHeat6 //smoke puff at startup, w/6 minutes of "heat" //startup=fx_F16ko_JetStartHeat9 //smoke puff at startup, w/9 minutes of "heat" ----------------------------------------------------------------------------------------------------------------- [LIGHTS]//retains all Kirk's original lights(except AB), list re-numbered, effects added... //#1=beacon #2=strobe #3=nav //#4=cockpit #5=landing #6=taxi //#7=recog #8=wing #9=logo //index,type, long, lat, vert, fx_filename //--------------------------------------------- light.0= 3, 12.2, 2.48, -1.4, fx_knavgre light.1= 3, 12.2, -2.48, -1.4, fx_knavred light.2= 3, -5.9, 16.70, 0.7, fx_knavgre light.3= 3, -5.9, -16.70, 0.7, fx_knavred light.4= 1, -19.1, 0.00, 3.3, fx_kbeaconwhite light.5= 1, -20.2, 0.00, 12.0, fx_kvbeacon light.6= 4, 15.6, 0.00, 3.5, fx_kvclight light.7= 3, 12.2, 2.48, -1.4, fx_kbeacongreen light.8= 3, 12.2, -2.48, -1.4, fx_kbeaconred light.9= 5, 15.0, 1.90, -7.9, fx_kLVIPER light.10=5, 25.0, 1.90, -5.9, fx_kLVIPER light.11=2, -12.6, 3.40, 1.1, fx_knavwhi light.12=2, -12.6, -3.40, 1.1, fx_knavwhi light.13=2, -14.6, -0.60, 3.1, fx_kLVIPER light.14=2, -14.6, 5.60, 3.1, fx_kLVIPER //----------afterburner effects------------------------ light.15=9, -19.70, 0.00, 0.0, fx_F16ko_BURN_ONE light.16=9, -19.70, 0.00, 0.0, fx_F16ko_BURN_TWO light.17=9, -22.30, 0.00, 0.0, fx_F16ko_TORCH_FLAME light.18=9, -18.00, 0.00, 0.0, fx_F16ko_GLITTER //----------------------------------------------------- ------------------------------------------------------------------------------------------------------- [SMOKESYSTEM] smoke.x=0.0, -5.9, 16.7, fx_kcontrail.fx smoke.x= 0.0, -5.9, -16.7, fx_kcontrail.fx smoke.0= 50, 1.0, -4.0, fx_kvapor.fx smoke.1= 50, 1.0, -6.0, fx_kvapor.fx smoke.2= 50., 1., 4.0, fx_kvapor.fx smoke.3= 50., 1., 6.0, fx_kvapor.fx smoke.4= 10., 1., 6.0, fx_kvapor_alt.fx smoke.5= 10., 1., 7.0, fx_kvapor_alt.fx smoke.6= 10., 1., -6.0, fx_kvapor_alt.fx smoke.7= 10., 1., -7.0, fx_kvapor_alt.fx smoke.x= -50.0, 0.0, 0.0, fx_smoke_w.fx ------------------------------------------------------------------------------------------------- [forcefeedback] stick_shaker_magnitude=15000 ; 0 - 10000 stick_shaker_direction=0 ; 0 - 35999 degrees stick_shaker_period=111111 ; in microseconds gear_bump_nose_magnitude=6000 ; 0 - 10000 gear_bump_nose_direction=18000 ; 0 - 35999 degrees gear_bump_nose_duration=250000 ; in microseconds gear_bump_left_magnitude=6000 ; 0 - 10000 gear_bump_left_direction=35500 ; 0 - 35999 degrees gear_bump_left_duration=250000 ; in microseconds gear_bump_right_magnitude=6000 ; 0 - 10000 gear_bump_right_direction=00500 ; 0 - 35999 degrees gear_bump_right_duration=250000 ; in microseconds ground_bumps_magnitude1=1500 ; 0 - 10000 ground_bumps_angle1=8900 ; 0 - 35999 degrees ground_bumps_intercept1=5.0 ground_bumps_slope1=0.48 ground_bumps_magnitude2=750 ; 0 - 10000 ground_bumps_angle2=9100 ; 0 - 35999 degrees 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 --------------------------------------------------------------------------------------------- [pitot_static] vertical_speed_time_constant = 100 ----------------------------------------------------------------------------------------------- [autopilot] autopilot_available=1 flight_director_available= 1 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 max_pitch=10.000000 max_pitch_acceleration=1.000000 max_pitch_velocity_lo_alt=2.000000 max_pitch_velocity_hi_alt=1.500000 max_pitch_velocity_lo_alt_breakpoint=20000.000000 max_pitch_velocity_hi_alt_breakpoint=28000.000000 max_bank=25.000000 max_bank_acceleration=1.800000 max_bank_velocity=3.000000 max_throttle_rate=0.100000 nav_proportional_control=9.000000 nav_integrator_control=0.250000 nav_derivative_control=0.000000 nav_integrator_boundary=2.500000 nav_derivative_boundary=0.000000 gs_proportional_control=9.520000 gs_integrator_control=0.260000 gs_derivative_control=0.000000 gs_integrator_boundary=0.700000 gs_derivative_boundary=0.000000 yaw_damper_gain=0.000000 [direction_indicators] direction_indicator.0=3,0 -------------------------------------------------------------------------------------------------- [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= 1.200 pitch_scalar= 1.000 flaps-position.0= 0.000, 0.000 flaps-position.1= 8.996, 0.000 flaps-position.2= 15.996, 0.000 flaps-position.3= 22.992, 0.000 ---------------------------------------------------------------------------------------- [Flaps.1] type= 2 span-outboard= 0.800 extending-time= 2.000 system_type= 0 damaging-speed= 250.000 blowout-speed= 300.000 lift_scalar= 0.700 drag_scalar= 0.100 pitch_scalar= 0.100 flaps-position.0= 0.000, 0.000 flaps-position.1= 0.000, 0.000 flaps-position.2= 18.000, 0.000 --------------------------------------------------------------------------------------------------------------- [TailHook] tailhook_length=4 ;(feet) tailhook_position=-15.0, 0.0, -1.0 ;(feet) longitudinal, lateral, vertical positions from datum cable_force_adjust=0.9 ------------------------------------------------------------------------------------------------------------------------------------------- [electrical] ;BusType, MaxAmpLoad, MinVoltage ;BusTypes:0=MainBus,1=AvionicsBus,2=BatteryBus,3=HotBatteryBus,4-7=Generator/AlternatorBus(1-4) max_battery_voltage=24.0 min_battery_voltage=24.0 max_generator_alternator_amps=400.0 generator_alternator_voltage=28.0 flap_motor = 0, 5 , 17.0 gear_motor = 0, 5 , 17.0 autopilot = 0, 5 , 17.0 avionics_bus = 0, 10, 17.0 avionics = 1, 5 , 17.0 pitot_heat = 0, 2 , 17.0 additional_system = 0, 20, 17.0 marker_beacon = 1, 2 , 17.0 gear_warning = 0, 2 , 17.0 fuel_pump = 0, 5 , 17.0 starter1 = 0, 20, 17.0 light_nav = 0, 5 , 17.0 light_beacon = 0, 5 , 17.0 light_landing = 0, 5 , 17.0 light_taxi = 0, 5 , 17.0 light_strobe = 0, 5 , 17.0 light_panel = 0, 5 , 17.0 --------------------------------------------------------------------------------------------------------- [flight_tuning] cruise_lift_scalar = 1.1 parasite_drag_scalar = 1.63 induced_drag_scalar = 1.0 elevator_effectiveness = 1.4 aileron_effectiveness = 1.3 rudder_effectiveness = 1.0 pitch_stability = 1.5 roll_stability = 1.2 yaw_stability = 1.2 elevator_trim_effectiveness = 1.0 aileron_trim_effectiveness = 1.0 rudder_trim_effectiveness = 1.0 --------------------------------------------------------------------------------------------------------- [Radios] // Radio Type = availiable, 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, 0 Adf.1 = 1 Transponder.1 = 1 Marker.1 = 1 --------------------------------------------------------------------------------------------------------- [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 ---------------------------------------------------------------------------------------------------------- [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=3,0 [brakes] toe_brakes_scale=0.671407 parking_brake=1 [gear_warning_system] gear_warning_available=0 pct_throttle_limit=0.000000 flap_limit_power=0.000000 flap_limit_idle=0.000000 [hydraulic_system] normal_pressure=0.000000 [stall_warning] type=1 [attitude_indicators] attitude_indicator.0=1 [turn_indicators] turn_indicator.0=1,0 [General] performance=0\n\n\n\n\n