[fltsim.0]
title=Gloster Meteor F Mk 8 Clean
sim=Trial Meteor
model=
panel=
sound=
texture=
checklists=
description=Gloster Meteor F Mk 8 VZ494\nDay Fighter of 501 Sqn  RAF based at Filton.\nAircraft design: Roger Hardy\[email protected]\nAir file:by Paolo Zamparo  [email protected]\nSounds:FS2K Lear 45. Panel: Dave Haskell\nV1.0 Date: March 2001\n\n\n
ui_manufacturer=Gloster
ui_type=Meteor F. Mk 8
ui_variation=VZ494 Clean Config
atc_airline=Air Force
atc_id=VZ494

[fltsim.1]
title=Gloster Meteor F Mk 8 with tanks
sim=Trial Meteor
model=Tanks
panel=
sound=
texture=
checklists=
description=Gloster Meteor F Mk 8 VZ494\nDay Fighter of 501 Sqn  RAF based at Filton.\nAircraft design: Roger Hardy\[email protected]\nAir file:by Paolo Zamparo  [email protected]\nSounds:FS2K Lear 45. Panel: Dave Haskell\nV1.0 Date: March 2001\n\n\n
ui_manufacturer=Gloster
ui_type=Meteor F. Mk 8
ui_variation=VZ494 Underwing Tanks
atc_airline=Air Force
atc_id=VZ494

[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 = 500
gear_bump_right_duration = 250000
ground_bumps_magnitude1 = 3250
ground_bumps_angle1 = 8900
ground_bumps_intercept1 = 5#
ground_bumps_slope1 = 0.48
ground_bumps_magnitude2 = 750
ground_bumps_angle2 = 9100
ground_bumps_intercept2 = 0.075
ground_bumps_slope2 = 1#
crash_magnitude1 = 10000
crash_direction1 = 1000
crash_magnitude2 = 10000
crash_direction2 = 9000
crash_period2 = 75000
crash_duration2 = 2500000

[General]
performance=Wing span 11.329 m---Length 13.59 m-- Powerplant one RR Derwent 8 rated at 3500 lb - Internal fuel capacity 420 gals\s max fuel 795 gals  MTOW 8648 kg (19065 lb) Max speed sea level 500 KTAS -\n

[WEIGHT_AND_BALANCE]
reference_datum_position     =  0.0000, 0.0000, 0.0000       // (feet) distance from FlightSim Reference position: (1/4 chord, centerline, waterline)
empty_weight_CG_position=0.000000,0.000000,0.000000
max_number_of_stations=50
station_load.0=0.000000,0.000000,0.000000,0.000000
empty_weight=12617.000000
empty_weight_roll_MOI=28000.000000
empty_weight_pitch_MOI=20000.000000
empty_weight_yaw_MOI=40000.000000
empty_weight_coupled_MOI=1300.000000

[fuel]
Center1=0.000000,0.000000,-2.333333,210.000000,0.000000
LeftMain=0.000000,0.000000,0.000000,252.000000,0.000000
LeftAux=0.000000,-12.833333,-2.583333,120.000000,0.000000
RightMain=0.000000,0.000000,0.000000,252.000000,0.000000
RightAux=0.000000,12.833333,-2.583333,120.000000,0.000000
fuel_type=2.000000
number_of_tank_selectors=1

[airplane_geometry]
wing_area=350.000000
wing_span=37.166667
wing_root_chord=9.416667
wing_dihedral=5.998535
wing_incidence=-0.494385
wing_twist=0.999756
oswald_efficiency_factor=1.668948
wing_winglets_flag=0
wing_sweep=0.000000
wing_pos_apex_lon=0.000000
wing_pos_apex_vert=0.000000
htail_area=40.000000
htail_span=15.000000
htail_pos_lon=-23.333333
htail_pos_vert=0.000000
htail_incidence=0.000000
htail_sweep=0.000000
vtail_area=29.000000
vtail_span=6.140033
vtail_sweep=0.000000
vtail_pos_lon=-23.333333
vtail_pos_vert=6.666667
elevator_area=14.600000
aileron_area=27.940000
rudder_area=8.200000
elevator_up_limit=27.501974
elevator_down_limit=20.626481
aileron_up_limit=19.480565
aileron_down_limit=14.896903
rudder_limit=23.491270
elevator_trim_limit=19.480565
spoiler_limit=59.988681
spoilerons_available=0
aileron_to_spoileron_gain=0.000000
min_ailerons_for_spoilerons=0.000000
min_flaps_for_spoilerons=0.000000

	//0  Class
        //1  Longitudinal Position        (feet)
        //2  Lateral Position             (feet)
        //3  Vertical Position            (feet)
        //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
        //10 Damping Ratio               (0=Undamped, 1=Critically Damped)
        //11 Extension Time              (seconds)
        //12 Retraction Time             (seconds)
        //13 Sound Type

[contact_points]
point.0=1, 14.98, -0.02, -6.21, 1574.803150,0.000000,1.31,40.080000,0.602862,2.500000,0.578249,5.000000,5.000000,0.000000,0.000000,0.000000
point.1=1, -1.63, -5.35, -6.11, 1574.803150,1.000000,1.31,0.000000,1.085730,2.500000,1.524227,5.000000,5.000000,2.000000,0.000000,0.000000
point.2=1, -1.63, 5.30, -6.11, 1574.803150,2.000000,1.31,0.000000,1.085730,2.500000,1.524227,5.000000,5.000000,3.000000,0.000000,0.000000
point.3=1.000000,14.000000,0.083333,-5.333333,1574.803150,0.000000,0.000000,0.000000,0.602862,2.500000,0.578249,0.000000,0.000000,1.000000,0.000000,0.000000
point.4=2.000000,0.000000,-18.166667,-0.750000,1574.803150,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,5.000000,0.000000,0.000000
point.5=2.000000,0.000000,18.166667,-0.750000,1574.803150,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,6.000000,0.000000,0.000000
point.6=2.000000,-26.000000,0.166667,0.333333,1574.803150,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,9.000000,0.000000,0.000000
point.7=2.000000,13.083333,0.000000,-2.083333,1574.803150,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,4.000000,0.000000,0.000000
static_pitch     = 0        //degrees (pitch when loaded on ground)
static_cg_height=5.904           //feet, altitude of CG when at rest on the ground

[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=19.996227,0.000000
flaps-position.2=39.992454,0.000000

[GeneralEngineData]
engine_type=1
Engine.0=0.000000,-7.583333,-1.166667
Engine.1=0.000000,7.583333,-1.166667
fuel_flow_scalar=1.000000

[TurbineEngineData]
fuel_flow_gain=0.002170
inlet_area=4.208640
rated_N2_rpm=29920.000000
static_thrust=3507.200000
afterburner_available=0
reverser_available=0

[Reference Speeds]
flaps_up_stall_speed=103.000000
full_flaps_stall_speed=82.400000
cruise_speed=331.930068

[keyboard_response]
elevator=150.000000,250.000000
aileron=150.000000,250.000000
rudder=150.000000,250.000000

[Views]
eyepoint=9.163283,0.000000,2.588788

[autopilot]
autopilot_available=1
flight_director_available=0
default_vertical_speed=1800.000000
autothrottle_available=1
autothrottle_arming_required=1
autothrottle_takeoff_ga=1
autothrottle_max_rpm=90.000000
pitch_takeoff_ga=8.000000

[direction_indicators]
direction_indicator.0=3,0