[fltsim.0]
title=(AMI) Aeritalia F-104S Starfighter (9-41)
sim=F-104S
model=
panel=
sound=
texture=
checklists=
kb_checklists=F-104S_Check
kb_reference=F-104S_Ref
ui_manufacturer=Aeritalia
ui_type=F-104S Starfighter
ui_variation=9° Stormo - 10° Gruppo
description=The F-104S is a develop of the original F-104G whit a more powerfull engine, stronger body structure, improvements to avionics and ordinance capabilities and two new lateral tail fins for better stability at high speeds. The F-104S was choosed by the Italian Air Force in 1966 to replace its fleet of F-104G. Almost all the 206 F-104S were directly produced in Italy by Aeritalia which produced also 40 aircrafts for the Turkish Air Force. This aircraft is from the 9th Wing "Francesco Baracca" of the 10th Group of the Italian Air Force (AMI) which received its first F-104S in early 1972. This F-104S has the "Europe Camo" color scheme as it appeared in 1970s and 1980s. Its primary role was interception and air superiority.
atc_heavy=0
atc_id=941
atc_airline=AMI
atc_flight_number=


[forcefeedback]
gear_bump_nose_magnitude=6000
gear_bump_nose_direction=18000
gear_bump_nose_duration=250000
gear_bump_left_magnitude=6000
gear_bump_left_direction=35500
gear_bump_left_duration=250000
gear_bump_right_magnitude=6000
gear_bump_right_direction=00500
gear_bump_right_duration=250000
ground_bumps_magnitude1=3250
ground_bumps_angle1=8900
ground_bumps_intercept1=5.0
ground_bumps_slope1=0.48
ground_bumps_magnitude2=750
ground_bumps_angle2=9100
ground_bumps_intercept2=0.075
ground_bumps_slope2=1.0
crash_magnitude1=10000
crash_direction1=01000
crash_magnitude2=10000
crash_direction2=9000
crash_period2=75000
crash_duration2=2500000

[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=50
station_load.0=0.000000,0.000000,0.000000,0.000000
empty_weight=14903.000
empty_weight_roll_MOI=55000.000
empty_weight_pitch_MOI=188000.000
empty_weight_yaw_MOI=180000.000
empty_weight_coupled_MOI=1300.000
max_gross_weight=22314.500
CG_forward_limit=0.000
CG_aft_limit=1.000

[fuel]
Center1=0.000, 0.000, 0.000, 179.000, 0.000
LeftMain=8.333, 0.000, 0.000, 179.000, 0.000
LeftAux=-4.167, 0.000, 0.000, 179.000, 0.000
RightMain=8.333, 0.000, 0.000, 179.000, 0.000
RightAux=-4.167, 0.000, 0.000, 179.000, 0.000
fuel_type=2.000
number_of_tank_selectors=1

[airplane_geometry]
wing_area=196.000
wing_span=21.917
wing_root_chord=8.917
wing_dihedral=-9.998
wing_incidence=-0.494
wing_twist=0.000
oswald_efficiency_factor=1.500
wing_winglets_flag=0
wing_sweep=0.000
wing_pos_apex_lon=0.000
wing_pos_apex_vert=0.000
htail_area=90.000
htail_span=11.917
htail_pos_lon=-18.750
htail_pos_vert=0.000
htail_incidence=0.000
htail_sweep=0.000
vtail_area=52.000
vtail_span=8.222
vtail_sweep=0.000
vtail_pos_lon=-16.667
vtail_pos_vert=5.833
elevator_area=22.500
aileron_area=7.840
rudder_area=9.350
elevator_up_limit=27.502
elevator_down_limit=20.626
aileron_up_limit=19.481
aileron_down_limit=14.897
rudder_limit=23.491
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]
point.0=1.000, 12.500, 0.000, -5.300, 1574.803, 0.000, 0.630, 39.000, 0.184, 2.500, 0.827, 5.000, 5.000, 0.000, 0.000, 0.000
point.1=1.000, -2.000, -4.167, -5.213, 1574.803, 1.000, 0.630, 0.000, 0.162, 2.500, 0.881, 5.000, 5.000, 2.000, 0.000, 0.000
point.2=1.000, -2.000, 4.167, -5.213, 1574.803, 2.000, 0.630, 0.000, 0.162, 2.500, 0.881, 5.000, 5.000, 3.000, 0.000, 0.000
point.3=2.000, -8.500, -11.083, -2.000, 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, -8.500, 11.083, -2.000, 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, -21.167, 0.000, -0.500, 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, 32.500, 0.000, -0.500, 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=4.001

[GeneralEngineData]
engine_type=1
Engine.0=-9.583, 0.000, 0.583
fuel_flow_scalar=1.000

[TurbineEngineData]
fuel_flow_gain=0.002
inlet_area=16.50
rated_N2_rpm=29920.000
static_thrust=17915.500
afterburner_available=0
reverser_available=0

[Reference Speeds]
flaps_up_stall_speed=150.000
full_flaps_stall_speed=120.000
cruise_speed=578.245

[keyboard_response]
elevator=150.000, 250.000
aileron=150.000, 250.000
rudder=150.000, 250.000

[Views]
eyepoint=17.10, 0.000, 2.8

[General]
performance=AMI Aeritalia F-104S Starfighter (9-41)\n\nLength: 54.8 ft\nHeight: 13.5 ft\nWing span: 21.9 ft\nMain Wing Area: 196.1 sq. ft\nEmpty Weight: 14,903 lbs\nMTOW: 30,997 lbs\nPower: 1 Fiat/General Electric J79-GE-19 x 17,915 lbs\nInternal Fuel Capacity: 897 US Gallons\nMax Speed: Mach 2,25+\nCruise Speed (economic): Mach 0.89 at 36,000 ft\nStall Speed: 198 mph\nService Ceiling: 64,795 ft\nNormal Range: 730 miles\nArmament: AIM-9B Sidewinder and AIM-7E Sparrow (Aspide) plus a large variety of air-to-ground weapons.\n\nAircraft by Michael Davies and Steve Bezant (Alpha Simulations).\nFlight Model and Package by Simone Pratticò.\nPanel rework by Simone Pratticò from an original by Marco Spada.\nSound Package by Mike hambly.\n\nE-Mail:\nMichael Davies and Steve Bezant (Alpha Simulations): phil@alphasim.co.uk\nSimone Pratticò: spratti@tin.it\nMarco Spada: m.spada@mclink.it\nMike Hambly: Bluearrowfs1@aol.com\n\nItaly, March 2002.\n\nDisclaimer: This Package is FREEWARE!!! DON'T MAKE MONEY WHIT IT!!!
atc_type=LOCKHEED
atc_model=F-104S

[autopilot]
autopilot_available=1
flight_director_available=0
default_vertical_speed=1800.000
autothrottle_available=1
autothrottle_arming_required=0
autothrottle_takeoff_ga=0
autothrottle_max_rpm=110.000
pitch_takeoff_ga=8.000
use_no_default_bank=1

[Flaps.0]
type=1
span-outboard=0.500
extending-time=5.000
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=13.331, 0.000
flaps-position.2=26.662, 0.000
flaps-position.3=39.992, 0.000

[direction_indicators]
direction_indicator.0=3,0