[fltsim.0]
title=Invader
sim=Invader
model=
panel=
sound=
texture=
atc_parking_types=RAMP
ui_manufacturer=Invader
ui_type=Invader
ui_variation=Standard
description=Recon Pre-Invasion craft, classification, landing craft, circular hull, 4 passenger.  This is a captured UFO disc craft or flying saucer.  Its propulsion system utilizes fusion technologies coupled with magnetic and gravitic force manipulation drive that uses a 'grey' field which is some what transdimensional being that magnetics exists in a parallel field, thus at times causing the vehicle to lose cohesion with this 'universe' or dimension, which also causes a 'mass' dilution where in the craft can travel tremendous speeds with hardly any energy as its weight dissipates to incredibly low and barely detectible mass amounts.
kb_checklists=



[General]
atc_type=
atc_model=
editable=1
performance=Length: 50feet\nSpan: 50 feet\nWeight: Max. 12,400 lbs.\nPower: Fusion Magnetic - Gravity Dimensional Drive \nRange: unknown, and unknown stats on the fusion reactor fuel lifespan as of yet.\nDesigner: William Ortis\nDate:August 2003\nOriginal designers of the Invaders Saucer are from the creators of the television show 'The Invaders'\n\n\n


[WEIGHT_AND_BALANCE]
max_gross_weight = 22000.0                      // (pounds)
empty_weight = 17000.0                          // (pounds)

reference_datum_position     =  1.0000, 0.0000, 0.0000       // (feet) distance from FlightSim Reference position: (1/4 chord, centerline, waterline)
empty_weight_CG_position     =  0, 0, 0    // (feet) longitudinal, lateral, vertical distance from specified datum

max_number_of_stations = 50

station_load.0  = "170, -17.0, -1.2, 0.0, Pilot"           // Weight(lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.10 = "100, -42.0,  0.0, 0.0, Baggage1"        // Weight(lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.11 =  "50, -45.0,  0.0, 0.0, Baggage2"        // Weight(lbs), longitudinal, lateral, vertical positions from datum (feet)

;Moments of Inertia
empty_weight_pitch_MOI  = 33000000
empty_weight_roll_MOI   = 12000000
empty_weight_yaw_MOI    =  7500000
empty_weight_coupled_MOI =  150000
reference_datum_position     =  0.0000, 0.0000, 0.0000       // (feet) distance from FlightSim Reference position: (1/4 chord, centerline, waterline)
empty_weight_CG_position=0.0, 0.0, 0.0
max_number_of_stations=50
station_load.0=0.000000,0.000000,0.000000,0.000000

[electrical]
max_battery_voltage = 12.0
generator_alternator_voltage = 13.8
max_generator_alternator_amps = 40.0

                ;BusType, MaxAmpLoad, MinVoltage       BusTypes:0=MainBus,1=AvionicsBus,2=BatteryBus,3=HotBatteryBus,4-7=Generator/AlternatorBus(1-4)
avionics_bus       = 0, 5 , 9.5
avionics           = 1, 5 , 9.5
additional_system  = 0, 2 , 9.5
marker_beacon      = 1, 2 , 9.0
fuel_pump          = 0, 5 , 9.0
engine_generator_map = 2,2

[flight_tuning]
cruise_lift_scalar     = 0.40
parasite_drag_scalar   = 1.0
induced_drag_scalar    = 1.5
elevator_effectiveness =4.00
aileron_effectiveness  = 0.50
rudder_effectiveness   = 6.0
pitch_stability        = 1.5
roll_stability         = 8.0
yaw_stability          = 1.0
elevator_trim_effectiveness = 1.0
aileron_trim_effectiveness  = 0.2
rudder_trim_effectiveness   = 8.0
spoiler_effectiveness  = 20.00


[GeneralEngineData]
engine_type = 1                                 //0=Piston, 1=Jet, 2=None, 3=Helo-Turbine, 4=Rocket, 5=Turboprop
Engine.0 = 0.0, -5.0, 0.0                       
Engine.1 = 0.0,  5.0, 0.0                     
fuel_flow_scalar        = 2.0                   //Scalar for fuel flow efficiency
min_throttle_limit = -0.35                      //Minimum percent throttle.  Generally negative for turbine reverser

[TurbineEngineData]
fuel_flow_gain          = 0.05                //Gain on fuel flow
inlet_area              = 6.0                //Square Feet, engine nacelle inlet area
rated_N2_rpm            = 29920                 //RPM, second stage compressor rated value
static_thrust           = 30000                  //Lbs, max rated static thrust at Sea Level
afterburner_available   = 1                     //Afterburner available?
reverser_available      = 1                     //Thrust reverser available?
prop_anim_ratio=-1.81 
gear_reduction_ratio=-45.500
[jet_engine]
thrust_scalar = 1.4


        //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, 22.00,   0.00,   -12.47, 1181.1, 0, 0.6349, 46.8, 0.3000, 2.5, 0.9100, 4.0, 4.0, 0, 260.0, 260.0
point.1=1, -17.25,  -15.75, -12.47, 1574.8, 1, 0.6349,  0.0, 0.4798, 2.5, 0.5456,  4.0,  4.0, 2, 260.0, 260.0
point.2=1, -17.25,   15.75, -12.47, 1574.8, 2, 0.6349,  0.0, 0.4798, 2.5, 0.5456,  4.0,  4.0, 3, 260.0, 260.0
point.3=2, -37.83, -23.92, -0.00,  787.4, 0, 0.0000,  0.0, 0.0000, 0.0, 0.0000,  0.0,  0.0, 5, 0.0, 0.0
point.4=2, -37.83,  23.92, -0.00,  787.4, 0, 0.0000,  0.0, 0.0000, 0.0, 0.0000,  0.0,  0.0, 6, 0.0, 0.0
point.5=2, -57.17,   0.00,  0.00,  787.4, 0, 0.0000,  0.0, 0.0000, 0.0, 0.0000,  0.0,  0.0, 9, 0.0, 0.0
point.6=2, -11.47,   0.00, -0.50,  787.4, 0, 0.0000,  0.0, 0.0000, 0.0, 0.0000,  0.0,  0.0, 4, 0.0, 0.0
point.7=4, -26.083333, 0.0, -3.70, 94200.0, 0.0, 0.693234, 0.0, 1.91, 2.5, 0.7470, 0.0, 0.0, 2.0, 0.0, 0.0
point.8=4, 22.083333, -20.0, -3.70, 94200.0, 0.0, 0.693234, 0.0, 1.91, 2.5, 0.7470, 0.0, 0.0, 3.0, 0.0, 0.0
point.9=4, 22.083333, 20.0, -3.70, 94200.0, 0.0, 0.693234, 0.0, 1.91, 2.5, 0.7470, 0.0, 0.0, 3.0, 0.0, 0.0
point.10=4, 26.083333, 0.0, -3.70, 94200.0, 0.0, 0.693234, 0.0, 1.91, 2.5, 0.7470, 0.0, 0.0, 3.0, 0.0, 0.0

static_pitch=0
static_cg_height=12.6
gear_system_type=1           //Hydraulic

[exits]
number_of_exits = 2
exit_rate.0 =0.275                     ;Percent per second
exit_rate.1 = 0.275                          ;Percent per second


[anemometers]
anemometer.0 = 0.0, 0.0, 4.7       //Position from Datum

[gear_warning_system]
gear_warning_available = 1    //Normal
pct_throttle_limit =  0.1     //Percent throttle that activates warning
flap_limit_idle    = 15.0     //Flap angle that activates warning at idle
flap_limit_power   = 30.0     //Flap angle that activates warning at above idle

[brakes]
parking_brake = 1       //Parking brake available
toe_brakes_scale = 3.0  //Brake scalar

[hydraulic_system]
normal_pressure = 3000.0    //PSI
electric_pumps  = 0         //no electric pumps
engine_map      = 1,1,0,0   //pumps on Eng1,2

[Views]
eyepoint = 5.385, 0.00, 6.012

[LIGHTS]
//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing
light.2  = 4, -5.385, 5.00, 6.012, fx_vclight,
light.3  = 4,  0.385, 0.00, 6.012, fx_vclight,
light.4  = 4, -6.385, 0.00, 6.012, fx_vclight,
light.5  = 4,  5.385, 6.00, 6.012, fx_vclight,
light.6  = 4,  5.385,-6.00, 6.012, fx_vclight,
light.7  = 4,  -0.385, -8.00, 6.012, fx_vclight,
light.8  = 4,  -0.385,  8.00, 6.012, fx_vclight,

[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

[flaps.0]
type             = 1                                    // 1 - tail, 2 - lead
span-outboard    = 0.8                                  // 0.0 .. 1.0
extending-time   = 6                                  // seconds
flaps-position.0 = 0                                    // degrees
flaps-position.1 = 5                                    // degrees
flaps-position.1 = 10                                    // degrees
flaps-position.1 = 15                                    // degrees
flaps-position.2 = 20                                   // degrees
flaps-position.3 = 40                                   // degrees
damaging-speed   = 1000                                  // KIAS
blowout-speed    = 1200                                  // KIAS
lift_scalar = 40.0 //1.5
drag_scalar = 18.0
pitch_scalar= 1.0
system_type = 1                                         //Hydraulic

[flaps.1]       //Outboard Leading Edge Slat
type             = 2                                    // 1 - tail, 2 - lead
span-outboard    = 0.8                                  // 0.0 .. 1.0
extending-time   = 8                                   // seconds
flaps-position.0 = 0                                    // 
flaps-position.1 = 0.5                                  // 
flaps-position.4 = 1.0                                  // 
damaging-speed   = 1000                                 // KIAS
blowout-speed    = 1200                                 // KIAS
lift_scalar = 30.0
drag_scalar = 10.0
pitch_scalar= 1.0
system_type = 1                                         //Hydraulic

[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

[attitude_indicators]
//Type: 0=None, 1=Vacuum Gyro, 2=Electric Gyro
attitude_indicator.0 = 2
attitude_indicator.1 = 1 

[turn_indicators]
//Type: 0=None, 1=Electric Gyro, 2= Vacuum Gyro
turn_indicator.0=0,0

[EFFECTS]
wake=fx_wake
water=fx_spray
dirt=fx_tchdrt
concrete=fx_sparks
touchdown=fx_tchdwn, 1

[fuel]
Center1   =  -11.4,   0.0, -1.5, 359.0, 0.0     //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)
LeftMain  =  -11.3, -10.0, -1.5, 268.5, 0.0     //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)
RightMain =  -11.3,  10.0, -1.5, 268.5, 0.0     //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)
fuel_type = 2                                   //Fuel type: 1 = Avgas, 2 = JetA
number_of_tank_selectors = 1
electric_pump=1

[airplane_geometry]
wing_area               = 3500.0                 //Square feet
wing_span               = 100.0                  //Feet
wing_root_chord         = 30.9                   //Feet
wing_dihedral           = 0.0                   //Degrees
wing_incidence          = 0.0                   //Degrees
wing_twist              = 0                     //Degrees
oswald_efficiency_factor= 1.00                   //Measure of lift effeciency of wing
wing_winglets_flag      = 1                     //Are winglets available?
wing_sweep              = 35.0                  //Degrees, wing leading edge
wing_pos_apex_lon       = 0.0                   //Feet, longitudinal distance from reference point, negative going aft
wing_pos_apex_vert      = 0.0                   //Feet, vertical distance from reference point, positive going up
htail_area              = 1200.0                //Square feet
htail_span              = 100.0                 //Feet
htail_pos_lon           = -50.0                 //Feet, longitudinal distance from reference point, negative going aft
htail_pos_vert          = 0.0                   //Feet, vertical distance from reference point, positive going up
htail_incidence         = 0.0                   //Degrees
htail_sweep             = 0.0                   //Degrees, horizontal tail leading edge
vtail_area              = 224.0                 //Square feet
vtail_span              = 20.0                  //Feet, tip to body
vtail_sweep             = 35.0                  //Degrees, vertical tail leading edge
vtail_pos_lon           = 0.0                   //Feet, longitudinal distance from reference point, negative going aft
vtail_pos_vert          = 0.0                   //Feet, vertical distance from reference point, positive going up
elevator_area           = 300.0                 //Square feet
aileron_area            = 300.0                 //Square feet
rudder_area             = 100.0                 //Square feet
elevator_up_limit       = 25.0                  //Degrees
elevator_down_limit     = 35.0                  //Degrees
aileron_up_limit        = 45.0                  //Degrees
aileron_down_limit      = 45.0                  //Degrees
rudder_limit            = 45.0                  //Degrees
elevator_trim_limit     = 30.0                  //Degrees
spoiler_limit           = 45.0                  //Degrees
spoilerons_available    =     0                //Spoilerons Available?
aileron_to_spoileron_gain =   3                 //Aileron to spoileron gain
min_ailerons_for_spoilerons = 10                //Degrees
min_flaps_for_spoilerons =    0                 //Minimum flap handle position when spoilerons activate
spoiler =  1

[Reference Speeds]
flaps_up_stall_speed    = 75.00                //Knots True (KTAS)
full_flaps_stall_speed  = 0.5           //Knots True (KTAS)
cruise_speed            = 1300                //Knots True (KTAS)
max_mach                = 3.00
max_indicated_speed     = 1400                   //Red line (KIAS)

[autopilot]
autopilot_available= 1
flight_director_available= 1
default_vertical_speed= 1800.0
autothrottle_available= 1
autothrottle_arming_required= 0
autothrottle_max_rpm = 90
autothrottle_takeoff_ga= 0
pitch_takeoff_ga = 8;
max_pitch=10.0
max_pitch_acceleration=1.0
max_pitch_velocity_lo_alt=2.0
max_pitch_velocity_hi_alt=1.5
max_pitch_velocity_lo_alt_breakpoint=20000.0
max_pitch_velocity_hi_alt_breakpoint=28000.0
max_bank=25.0
max_bank_acceleration=1.8
max_bank_velocity=3.00
max_throttle_rate=0.10
nav_proportional_control=11.00
nav_integrator_control=0.20
nav_derivative_control=0.00
nav_integrator_boundary=2.50
nav_derivative_boundary=0.00
gs_proportional_control=9.52
gs_integrator_control=0.26
gs_derivative_control=0.00
gs_integrator_boundary=0.70
gs_derivative_boundary=0.00
yaw_damper_gain = 1.0

[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

[stall_warning]
type=2

[propeller]
propeller_type=1
propeller_diameter=6.883000
propeller_blades=2
propeller_moi=5.706520
beta_max=0.000000
beta_min=15.000000
min_gov_rpm=0.000000
prop_tc=0.100000
gear_reduction_ratio=1.000000
fixed_pitch_beta=20.000000
low_speed_theory_limit=80.000000
prop_sync_available=0
prop_deice_available=0
prop_feathering_available=0
prop_auto_feathering_available=0
min_rpm_for_feather=0.000000
beta_feather=0.000000
power_absorbed_cf=0.000000
defeathering_accumulators_available=0
prop_reverse_available=0.000000
minimum_on_ground_beta=0.000000
minimum_reverse_beta=0.000000