[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