[fltsim.0]
title=Tornado_ADV-21°
sim=Tornado_ADV-21°
model=
panel=
sound=
texture=
checklists=
ui_manufacturer=Panavia
ui_type=ADV
ui_variation=ADV 21° Tiger-Group.
description=Tornado ADV  is the  Air Defence Variant of Tornado optimised for long range interception. Built by the Panavia consortium of three nations industries, British Aerospace-DASA (Germany)- Alenia (Italy).First flight, 27 October 1979.\nDesigner (visual FSDS model and texture): Giovanni Clemente. Country:  Novara ITALY.                          Web: WWW.GIOCLEM:COM\nem@il: fsgioclem@virgilio.it                                     Giugno 2002.                                                      Credit: Maxtac
atc_heavy=0
atc_id=
atc_airline=
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

[fltsim.1]
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[fltsim.2]
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[fltsim.3]
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[fltsim.5]
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[fltsim.6]
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[fltsim.7]
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[fltsim.8]
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[fltsim.9]
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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=50
station_load.0=0.000000,0.000000,0.000000,0.000000
empty_weight=28000.000
empty_weight_roll_MOI=238163.000
empty_weight_pitch_MOI=270219.000
empty_weight_yaw_MOI=383883.000
empty_weight_coupled_MOI=1300.000
max_gross_weight=45420.000
CG_forward_limit=0.000
CG_aft_limit=1.000

[fuel]
LeftMain=0.000, 0.000, 0.000, 1000.000, 0.000
LeftAux=0.000, 0.000, 0.000, 300.000, 0.000
RightMain=0.000, 0.000, 0.000, 1000.000, 0.000
RightAux=0.000, 0.000, 0.000, 300.000, 0.000
fuel_type=2.000
number_of_tank_selectors=1

[airplane_geometry]
wing_area=525.000
wing_span=38.333
wing_root_chord=13.667
wing_dihedral=2.999
wing_incidence=-0.494
wing_twist=-1.000
oswald_efficiency_factor=0.750
wing_winglets_flag=0
wing_sweep=0.000
wing_pos_apex_lon=0.000
wing_pos_apex_vert=0.000
htail_area=80.000
htail_span=16.667
htail_pos_lon=-23.333
htail_pos_vert=0.000
htail_incidence=0.000
htail_sweep=0.000
vtail_area=60.000
vtail_span=8.832
vtail_sweep=0.000
vtail_pos_lon=-20.000
vtail_pos_vert=5.833
elevator_area=20.000
aileron_area=21.000
rudder_area=10.200
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=1.00, 12.75,  0.00, -7.20,   1574.80, 0.0, 0.780208,42.00, 0.45, 2.50, 0.90, 4.0, 4.0, 0.0,  200.00,  200.00
point.1=1.00, -5.917,-5.25, -7.05,    1574.80, 1.00,0.780208, 0.00, 0.50, 2.50, 0.85, 5.0, 5.0, 2.0, 200.00, 200.00
point.2=1.00, -5.917, 5.25, -7.05,    1574.80, 2.00,0.780208, 0.00, 0.50, 2.50, 0.85, 5.0, 5.0, 3.0, 200.00,  200.00
point.3=2.000000,-18.083333,-15.583333,-0.166667,1574.803150,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,5.000000,0.000000,0.000000
point.4=2.000000,-18.083333,15.583333,-0.166667,1574.803150,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,6.000000,0.000000,0.000000
point.5=2.000000,-24.250000,0.000000,-2.000000,1574.803150,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,9.000000,0.000000,0.000000
point.6=2.000000,26.750000,0.000000,-2.000000,1574.803150,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,4.000000,0.000000,0.000000
static_pitch=0.000
static_cg_height=7.259

[GeneralEngineData]
engine_type=1
Engine.0=-13.333, -2.500, -1.667
Engine.1=-13.333, 2.500, -1.667
fuel_flow_scalar=1.000

[TurbineEngineData]
fuel_flow_gain=0.002
inlet_area=21.520
rated_N2_rpm=29920.000
static_thrust=17933.300
afterburner_available=0
reverser_available=1

[Reference Speeds]
flaps_up_stall_speed=120.000
full_flaps_stall_speed=96.000
cruise_speed=756.622

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

[Views]
eyepoint=13.561, 0.00, 3.373


[General]
performance=Length:18.68m Span:min 8.60 m \/ max 13.91 m\nWeight: MTOW 27986 kg - Empty  14502 kg\nPower:2 Turbo Union RB-199 Turbofan\nDesigner (visual FSDS model and texture): Giovanni Clemente. Country:  Novara ITALY.                          Web: WWW.GIOCLEM:COM\nem@il: fsgioclem@virgilio.it                                     Febbraio 2002.                                                      Credit: Maxtac for the spectacular  mouving parts.  WWW.MAXTAC.IT                              \n\n
atc_type=
atc_model=

[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=90.000
pitch_takeoff_ga=8.000

[Flaps.0]
type=1
span-outboard=0.500000
extending-time=5.000000
system_type=0
flaps-position.0=0.000000,0.000000
flaps-position.1=15.996982,0.000000
flaps-position.2=39.992454,0.000000

[smokesystem]
smoke.0=-1.00, -2.00, 3.750, fx_smoke_rx
smoke.1=-1.00, -2.00, -3.750, fx_smoke_rx

[LIGHTS]
//types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing 
//(feet) longitudinal, lateral, vertical distance from reference datum

light.0=3,  5.817,  5.840, 1.462, fx_navgreh ,
       
light.1=3,  5.817, -5.840, 1.462, fx_navredh ,
light.2=3,-30.273,  0.073, 11.941, fx_navwhih ,
light.3=3,-30.273, -0.073, 11.941, fx_navwhih ,
light.4=1,   7.850,  0.00, -2.845,  fx_beaconh ,
light.5=1,  -2.388,  0.00,  4.207,  fx_beaconh ,

[direction_indicators]
direction_indicator.0=3,0