----------------------------------F-16 VIPER (By KIRK OLSSON) ----------------------------------
[fltsim.0]
title=Viper_NOR
sim=Viper_NOR
model=
panel=
sound=
texture=
checklists=
description= F-16A MLU M4 Fighting Falcon of the Royal Norwegian Air Force. The MLU M4 updates introduces a software tape enabling the aircraft to carry and deliver the latest air to ground munitions like the JDAM. In addition to the already advanced and highly capable AIM-120 AMRAAM, the super agile IRIS-T short range air-to-air missile has been introduced, replacing the AIM-9L Sidewinder. The Pantera targeting pod makes a new dimension in Air to Ground missions used together with the new HMCS (Helmet Mounted Cueing System). The Pylon Integrated Dispenser System has the ALQ-162 ECM pod built-in and complements ALQ-131 ECM pod, carried on the centre line. PIDS also enables carriage of more chaff, housed in the pylon. \n---by Kirk Olsson---
ui_manufacturer=Lockheed Martin
ui_type=F-16A MLU M4 (Royal Norwegian Air Force)
ui_variation=a2a/a2g
atc_heavy=0
atc_id=664
atc_airline=Air Force
atc_flight_number=664
atc_parking_types=MIL_COMBAT
--------------------------------------------------
[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)
atc_type=LOCKHEED
atc_model=F16
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[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 = "220.0, 0.0, 15.0, -0.3, left wingtip" //Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.1 = "190.0, 0.0, 13.0, -0.5, left pylon 1" //Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.2 = "600.0, 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 = "750.0, 3.0, 0.0, -2.5, center pylon " //Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.6 = "500.0, 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 = "600.0, 0.5, -11.0, -0.5, right pylon 5" //Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.9 = "190.0, 0.0, -13.0, -0.5, right pylon 6" //Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.10 = "220.0, 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
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[fuel]
Center1= 0.000, 0.000, 0.000, 150.000, 0.000
LeftMain= 0.000, 0.000, 0.000, 350.000, 0.000
LeftAux= 0.000, -5.000, 0.000, 100.000, 0.000
LeftTip= 0.000, -10.000, 0.000, 0.000, 0.000
RightMain= 0.000, 0.000, 0.000, 350.000, 0.000
RightAux= 0.000, 5.000, 0.000, 100.000, 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
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[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
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[contact_points]
1 2 3 4 5 6 7 8 9 10
point.0= 1.000, 10.583, 0.000, -6.180, 1574.803, 0.000, 0.978, 37.620, 0.220, 1.700, 1.0, 6.300, 6.200, 0.000, 400.000, 0.000
point.1= 1.000, -2.500, -4.167, -6.430, 1574.803, 1.000, 1.000, 0.000, 0.605, 1.300, 1.2, 5.5, 5.600, 2.000, 400.000, 0.000
point.2= 1.000, -2.500, 4.167, -6.430, 1574.803, 2.000, 1.000, 0.000, 0.605, 1.300, 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
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[jet_engine]
thrust_scalar=1.0
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[GeneralEngineData]
engine_type= 1
Engine.0= -6.667, 0.000, 0.000
fuel_flow_scalar= 1.000
min_throttle_limit=0.000000
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[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
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[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
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[Views]
eyepoint=15.4,-0.02000,3.68
VIEW_FORWARD_ZOOM=0.00
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[exits]
number_of_exits=2
exit_rate.0=0.2 ;Percent per second
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[folding_wings]
wing_fold_system_type=4 ;0=None
fold_rates=0.52,0.22 ;Percent per second
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[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
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[EFFECTS]
wake=fx_wake
water=fx_spray
dirt=fx_tchdrt
concrete=fx_sparks
touchdown=fx_ktchdwn, 1
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[LIGHTS]
//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing
light.7=3, 12.2, 2.48, -1.4, fx_knavgre ,
light.5=3, 12.2, -2.48, -1.4, fx_knavred ,
light.6=3, -5.9, 16.7, 0.7, fx_knavgre
light.4=3, -5.9, -16.7, 0.7, fx_knavred
light.2=3, 12.2, 2.48, -1.4, fx_kbeacongreen ,
light.1=3, 12.2, -2.48, -1.4, fx_kbeaconred ,
light.8=5, 15.0, 1.9, -7.9, fx_kLVIPER ,
light.10=5, 25.0, 1.9, -5.9, fx_kLVIPER ,
light.11=4, -12.6, 3.4, 1.1, fx_knavwhi ,
light.12=4, -12.6, -3.4, 1.1, fx_knavwhi ,
light.13=4, -14.6, -0.6, 3.1, fx_kLVIPER ,
light.14=4, -14.6, 5.6, 3.1, fx_kLviper ,
light.3=1, -20.217, 0.0, 11.987, fx_kVbeacon ,
light.15= 4, 15.56, 0.00, 3.5, fx_kvclight ,
light.16=3, -21.4, 0.0, 4.5, fx_kbeaconwhite ,
light.20=4, 17.0, 2.9, -5.9, fx_kLVIPER ,
light.=21=4, 17.0, 2.9, -5.9, fx_kLVIPER
light.9=2, -18.2, 0.0, 0.3, fx_f1light.fx
light.xx=2, -20.8, 0.0, 0.3, fx_f1light.fx
light.xx=2, -23.2, 0.0, 0.3, fx_f1light.fx
light.xx=2, -25.2, 0.0, 0.3, fx_f1light.fx
light.xx= 4, 9.5, 0.00, 3.5, fx_kvclight ,
light.17=2, -15.2, 0.0, 0.531, fx_f1light.fx
light.18=2, -15.2, 0.0, 0.531, fx_f1lighta.fx
light.19=2, -15.2, 0.0, 0.531, fx_f1light.fx
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[SMOKESYSTEM]
smoke.9=0.0, -5.9, 16.7, fx_kcontrail.fx
smoke.10= 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.8= -50.0, 0.0, 0.0, fx_kf16exhaust.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
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[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
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[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