[fltsim.0]
title=Venture Vortex 2002
sim=USAF_C-32A
model=
panel=
sound=
texture=
panel_alias=
sound_alias=
kb_checklists=
kb_reference=
atc_id=80
atc_id_color=0xffffffff
atc_airline=Flag Ship
atc_flight_number=
ui_manufacturer=Boeing
ui_type=757-200
ui_variation=Venture Vortex
description=The first ever Boy Scout aircraft.  This plane is totaly fictional.  If it were real its purpose would serve as a transport for the equipment and staff for the Venture Vortex.  GMAX model by Mike Stone, authentic textures by Kevin Stewart.
atc_heavy=1

[General]
atc_type=BOEING AIRCRAFT
atc_model=B752
editable=1
performance=Max cruising speed 914km\/h (493kt)\nCruising speed 850km\/h (460kt). \nRange with P&W engines and 186 passengers 5053km (2728nm),

[pitot_static]
vertical_speed_time_constant=1                //Increasing this value will cause a more instantaneous reaction in the VSI


[WEIGHT_AND_BALANCE]
max_gross_weight= 220000.000
empty_weight= 125750.000

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= 19000.000, 0.000, 0.000, 0.000

;Moments of Inertia
empty_weight_pitch_MOI= 10000000.000
empty_weight_roll_MOI= 2000000.000
empty_weight_yaw_MOI= 6000000.000
empty_weight_coupled_MOI= 0.000
CG_forward_limit= 0.000
CG_aft_limit= 1.000

[flight_tuning]
cruise_lift_scalar=1.000
parasite_drag_scalar=1.000
induced_drag_scalar=1.000
elevator_effectiveness=1.000
aileron_effectiveness=1.000
rudder_effectiveness=1.000
pitch_stability=2.002
roll_stability=1.000
yaw_stability=1.000
elevator_trim_effectiveness=0.502
aileron_trim_effectiveness=1.000
rudder_trim_effectiveness=1.000

[SMOKESYSTEM]      
smoke.0=90.0,-27.3,-61.0, fx_WingVortex
smoke.1=90.0,-27.3,-48.0, fx_WingVortex
smoke.2=90.0,-27.3,48.0, fx_WingVortex
smoke.3=90.0,-27.3,61.0, fx_WingVortex

[GeneralEngineData]
engine_type= 1
Engine.0= 0.000, -22.000, -6.000
Engine.1= 0.000, 22.000, -6.000
fuel_flow_scalar= 1.000

[TurbineEngineData]
fuel_flow_gain= 0.002
inlet_area= 24.000
rated_N2_rpm= 29920.000
static_thrust= 37400.000
afterburner_available= 0
reverser_available= 1

[jet_engine]
thrust_scalar=1.000

[electrical]
;BusType, MaxAmpLoad, MinVoltage       BusTypes:0=MainBus,1=AvionicsBus,2=BatteryBus,3=HotBatteryBus,4-7=Generator/AlternatorBus(1-4)
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

//0  Class                        <0=none,1=wheel, 2=scrape, 3=float>
//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
//14 Airspeed limit for retraction     (KIAS)
//15 Airspeed that gear gets damage at (KIAS)

[contact_points]
point.0= 1.000, 40.000, 0.000, -12.300, 1181.100, 0.000, 1.442, 55.920, 0.800, 2.500, 0.900, 4.000, 4.000, 0.000, 0.000, 0.000
point.1= 1.000, -7.750, -8.580, -12.800, 1574.800, 1.000, 1.442, 0.000, 1.000, 2.500, 0.900, 6.900, 6.900, 2.000, 0.000, 0.000
point.2= 1.000, -7.750, 8.580, -12.800, 1574.800, 2.000, 1.442, 0.000, 1.000, 2.500, 0.900, 7.100, 7.100, 3.000, 0.000, 0.000

point.3= 2.000, -14.170, -47.330, -10.000, 787.400, 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, -14.170, 47.330, 0.000, 787.400, 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, -54.000, 0.000, 2.830, 787.400, 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, 42.670, 0.000, -3.750, 787.400, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 4.000, 0.000, 0.000

max_number_of_points=21

static_pitch= 0.620
static_cg_height= 11.500

[Views]
eyepoint=43.7, -1.31, 3.55   //(feet) longitudinal, lateral, vertical distance from reference datum





[Radios]
// Radio Type=availiable, standby frequency, has glide slope
Audio.1=1
Com.1=1, 1
Com.2=1, 1
Nav.1=1, 1, 1
Nav.2=1, 1, 0
Adf.1=1
Transponder.1=1
Marker.1=1

[LIGHTS]        
//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing
light.0=3, -24.31, -62.04,  3.97, fx_navredm ,
light.1=3, -24.31,  62.04,  3.97, fx_navgrem ,
light.2=3, -86.15,   0.00,  6.30, fx_navwhih ,
light.3=2, -21.59, -61.95,  4.00, fx_strobeh ,
light.4=2, -21.59,  61.95,  4.00, fx_strobeh ,
light.5=1,   5.38,   0.00, -6.21, fx_beaconb ,
light.6=1,  29.30,   0.00,  9.79, fx_beaconh ,
light.7=4,  61.43,   0.00,  5.36, fx_vclight ,

[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

[exits]
number_of_exits=2
exit_rate.0=0.4                               ;Percent per second
exit_rate.1=0.4                               ;Percent per second

[EFFECTS]
wake=fx_wake_ss
//water=fx_spray
water=fx_waterland
dirt=fx_tchdrt
concrete=fx_sparks
;touchdown=fx_tchdwn_s, 1

[autopilot]
autopilot_available=1
flight_director_available=1
default_vertical_speed=1800
autothrottle_available=1
autothrottle_arming_required=1
autothrottle_max_rpm=90
autothrottle_takeoff_ga=1
pitch_takeoff_ga=8;

[fuel]
Center1= 0.000, 0.000, 0.000, 5000.000, 0.000
LeftMain= -3.000, -19.000, 0.000, 3600.000, 0.000
RightMain= -3.000, 19.000, 0.000, 3600.000, 0.000
fuel_type=2                                   //Fuel type: 1 = Avgas, 2 = JetA
number_of_tank_selectors=1                    

[airplane_geometry]
wing_area= 1994.000
wing_span= 124.000
wing_root_chord= 25.000
wing_dihedral= 5.000
wing_incidence= 1.000
wing_twist= -0.500
oswald_efficiency_factor= 0.750
wing_winglets_flag= 0
wing_sweep= 25.000
wing_pos_apex_lon= 8.000
wing_pos_apex_vert= 0.000
htail_area= 600.000
htail_span= 52.000
htail_pos_lon= -70.000
htail_pos_vert= 4.000
htail_incidence= 0.000
htail_sweep= 30.000
vtail_area= 360.000
vtail_span= 24.000
vtail_sweep= 35.000
vtail_pos_lon= -70.000
vtail_pos_vert= 10.000
elevator_area= 84.000
aileron_area= 28.000
rudder_area= 120.000
elevator_up_limit= 22.500
elevator_down_limit= 19.500
aileron_up_limit= 20.000
aileron_down_limit= 20.000
rudder_limit= 26.000
elevator_trim_limit= 20.000
spoiler_limit= 60.000
spoilerons_available= 1
aileron_to_spoileron_gain= 3.000
min_ailerons_for_spoilerons= 10.000
min_flaps_for_spoilerons= 0.000

[Reference Speeds]
flaps_up_stall_speed= 142.000
full_flaps_stall_speed= 113.000
cruise_speed= 477.000


[forcefeedback]
gear_bump_nose_magnitude=3000           ; 0 - 10000
gear_bump_nose_direction=18000          ; 0 - 35999 degrees
gear_bump_nose_duration=250000          ; in microseconds
gear_bump_left_magnitude=2700           ; 0 - 10000
gear_bump_left_direction=35500          ; 0 - 35999 degrees
gear_bump_left_duration=250000          ; in microseconds
gear_bump_right_magnitude=2700          ; 0 - 10000
gear_bump_right_direction=00500         ; 0 - 35999 degrees
gear_bump_right_duration=250000         ; in microseconds
ground_bumps_magnitude1=1300            ; 0 - 10000
ground_bumps_angle1=08900               ; 0 - 35999 degrees
ground_bumps_intercept1=3.0
ground_bumps_slope1=0.20
ground_bumps_magnitude2=200             ; 0 - 10000
ground_bumps_angle2=09100               ; 0 - 35999 degrees
ground_bumps_intercept2=1.075
ground_bumps_slope2=0.035
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

[Flaps.0]
type= 1
span-outboard= 0.300
extending-time= 8.000
system_type= 1
damaging-speed= 250.000
blowout-speed= 300.000
lift_scalar= 1.000
drag_scalar= 1.000
pitch_scalar= 1.000
flaps-position.0= 0.000, 0.000
flaps-position.1= 1.000, 0.000
flaps-position.2= 5.000, 0.000
flaps-position.3= 15.000, 0.000
flaps-position.4= 20.000, 0.000
flaps-position.5= 25.000, 0.000
flaps-position.6= 30.000, 0.000

[Flaps.1]
type= 1
span-outboard= 0.400
extending-time= 8.000
system_type= 1
damaging-speed= 250.000
blowout-speed= 300.000
lift_scalar= 1.000
drag_scalar= 1.000
pitch_scalar= 1.000
flaps-position.0= 0.000, 0.000
flaps-position.1= 1.000, 0.000
flaps-position.2= 5.000, 0.000
flaps-position.3= 15.000, 0.000
flaps-position.4= 20.000, 0.000
flaps-position.5= 25.000, 0.000
flaps-position.6= 30.000, 0.000

[Flaps.2]
type= 2
span-outboard= 0.800
extending-time= 2.000
system_type= 1
damaging-speed= 250.000
blowout-speed= 300.000
lift_scalar= 1.000
drag_scalar= 1.000
pitch_scalar= 1.000
flaps-position.0= 0.000, 0.000
flaps-position.1= 1.000, 0.000