;SS ADVENTURE ;By Phil Crowther ;SOURCE ;FourEngineJet.cfg/air [fltsim.0] title=SS Adventure sim=ss_adventure model= panel= sound= texture= kb_checklists=ss_adventure_check kb_reference=ss_adventure_ref ui_manufacturer=FS Shipyards.org ui_type=SS Adventure ui_variation= description=The Adventure is the sister ship to the Venture, a ship lost while enroute to Skull island. [General] atc_type= atc_model= editable=1 performance= Category=airplane [Reference Speeds] flaps_up_stall_speed = 040 full_flaps_stall_speed = 000 cruise_speed = 011 max_indicated_speed = 040 max_mach = 0.919971 [WEIGHT_AND_BALANCE] max_gross_weight = 875000 empty_weight = 401100 reference_datum_position = 0,0,0 ;ZXY distance from FlightSim Reference empty_weight_CG_position = 0,0,0 ;ZXY distance from specified datum max_number_of_stations = 10 station_load.0 = 40000, 0,0,0 ;Payload Weight, ZXY position from datum ;Moments of Inertia empty_weight_pitch_MOI = 96304110 ;originally 24223159 empty_weight_roll_MOI = 15352310 ;computed as 672647 empty_weight_yaw_MOI = 32167308 ;originally 39531785 empty_weight_coupled_MOI = 0 [contact_points] ; 0 Class (4=floats) ; 1 Longitudinal Position (feet) [BIGGER = SLOWER WAVE MOTION + NOSE PLOWS] ; 2 Lateral Position (feet) [BIGGER CREATES VIBRATION] ; 3 Vertical Position (feet) [MORE POSITIVE = LOWER] ; 4 Impact Damage Threshold (Feet Per Minute) ; 5 Brake Map (0=None, 1=Left, 2=Right) [N/A] ; 6 Wheel Radius (feet) ; 7 Steer Angle (degrees) [CHANGE THIS TO MAKE SHIP TURN FASTER] ; 8 Static Compression (feet) (0=rigid) ; 9 Max/Static Compression Ratio ;10 Damping Ratio/Water Rudder Effectiveness (0=Undamped, 1=Critically Damped) ;11 Extension Time (seconds) [N/A TO FIXED GEAR] ;12 Retraction Time (seconds) [N/A TO FIXED GEAR] ;13 Sound Type [WATER SOUND?] ;14 Airspeed limit for retraction (KIAS) [N/A TO FIXED GEAR] ;15 Airspeed that gear gets damage at (KIAS) [N/A TO FIXED GEAR] ; 0 1 2 3 4 5 6 7 8 9 10 11 12 13 14 15 ; 0 Z X Y FPM BM WR SA SC Max DR ET RT SND RL GD point.0=4, 40,-08, -4.5, 9999, 0, 1, 05, 0.9, 15.5, 0.65, 00, 00, 2, 00, 00 point.1=4, 40, 08, -4.5, 9999, 0, 1, 05, 0.9, 15.5, 0.65, 00, 00, 3, 00, 00 point.2=4,-40,-08, -4.5, 9999, 0, 1, 00, 0.9, 15.5, 0.65, 00, 00, 2, 00, 00 point.3=4,-40, 08, -4.5, 9999, 0, 1, 00, 0.9, 15.5, 0.65, 00, 00, 3, 00, 00 point.4=1, 0, 0, -5.0, 9999, 0, 1, 00, 0.9, 15.5, 0.65, 05, 05, 3, 00, 00 ;FOR HORN static_pitch = 0.0 static_cg_height = 4.0 ;[MUST BE POS #, OR FLIES INTO SPACE] gear_system_type = 0 ;Hydraulic [FOR HORN] [Views] ;ZXY distance from reference datum (feet) ;eyepoint = 0.00, 0.00, 20.70 ;wheelhouse eyepoint = 0.00, 0.90, 20.70 ;wheelhouse - offset to the right [LIGHTS] ;type, longitudinal, lateral, vertical distance from ref datum, name ;Light types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing ;adjust these positions as you would for the [Views] section ;---internal (flying deck) light.0 = 4, 01.68, 00.15, 20.650, fx_vclighth ;high panel/VC-lighting light.1 = 4, 01.68, 00.15, 20.650, fx_vclight ;normal panel/VC-lighting ;---external light.2 = 3, 9.250, -13.10, 16.000, fx_navred ;cabin left light.3 = 3, 9.250, 13.10, 16.000, fx_navgre ;cabin right light.4 = 3, 62.123, 00.00, 41.725, fx_navwhi ;foremast light.6 = 3, -31.483, 00.00, 41.725, fx_navwhi ;mizzenmast light.7 = 3, -70.675, 00.00, 20.250, fx_navwhi ;flagstaff light.8 = 3, 2.000, 00.00, 27.000, fx_navwhi ;flying deck [EFFECTS] wake = fx_wake_ijt1 water =ian [SMOKESYSTEM] ;This is enabled by gauge Y-not work, Z, X smoke.0 = 0.00, 0.00,0.00,fx_ssmoke13 ;black smoke smoke.1 = 85.00, 3.0,00.00, fx_spray1.fx ;bow smoke.2 = 85.00, -3.0, 00.00, fx_spray1.fx ;bow smoke.3 = 88.00, 00.0, 0.00, fx_spray1.fx ;bow [flight_tuning] cruise_lift_scalar = 0.000 ;changed from 1 to 0 parasite_drag_scalar = 1.000 induced_drag_scalar = 1.000 elevator_effectiveness = 0.000 ;changed from 1 to 0 aileron_effectiveness = 0.000 ;changed from 1 to 0 rudder_effectiveness = 0.000 ;changed from 1 to 0 pitch_stability = 1.000 roll_stability = 1.000 yaw_stability = 1.000 elevator_trim_effectiveness = 0.000 ;changed from 1 to 0 aileron_trim_effectiveness = 0.000 ;changed from 1 to 0 rudder_trim_effectiveness = 0.000 ;changed from 1 to 0 [airplane_geometry] ;[NO CHANGES] wing_area = 5825.0 ;Square feet wing_span = 211.4 wing_root_chord = 48.8 wing_dihedral = 7.0 ;Degrees wing_incidence = 2.0 ;Degrees wing_twist = -1.0 ;Degrees oswald_efficiency_factor = 0.68 ;Measure of lift effeciency of wing wing_winglets_flag = 1 ;Are winglets available? wing_sweep = 37.5 ;Degrees, wing leading edge wing_pos_apex_lon = -68.2 ;Z distance from ref point wing_pos_apex_vert = 0 ;Y distance from ref point htail_area = 1470 ;Square feet htail_span = 72.8 htail_pos_lon = -210.0 ;Z distance from ref point htail_pos_vert = 0.0 ;Y distance from ref point htail_incidence = 0.0 ;Degrees htail_sweep = 37.5 ;horizontal tail leading edge vtail_area = 1060 ;Square feet vtail_span = 37.1 ;tip to body vtail_sweep = 45.0 ;Degrees, vertical tail leading edge vtail_pos_lon = -198.5 ;Z distance from ref point vtail_pos_vert = 26.1 ;Y from ref point elevator_area = 327 ;Square feet aileron_area = 225 ;Square feet rudder_area = 230 ;Square feet elevator_up_limit = 25 ;Degrees elevator_down_limit = 15 ;Degrees aileron_up_limit = 25 ;Degrees aileron_down_limit = 15 ;Degrees rudder_limit = 31.5 ;Degrees elevator_trim_limit = 20 ;Degrees spoiler_limit = 45 ;Degrees spoilerons_available = 1 ;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 auto_spoiler_available=0 spoiler_extension_time=2.000000 positive_g_limit_flaps_up=4.000000 positive_g_limit_flaps_down=3.000000 negative_g_limit_flaps_up=-3.000000 negative_g_limit_flaps_down=-2.000000 ;[flaps.0] ;type = 0 [flaps.0] type = 1 ;(1 - tail) span-outboard = 0.8 ;0.0 .. 1.0 extending-time = 2 ;seconds flaps-position.0 = 0 ;degrees flaps-position.1 = 1 ;degrees damaging-speed = 120 ;KIAS blowout-speed = 150 ;KIAS lift_scalar = 0.0 drag_scalar = 0.0 pitch_scalar = 0.0 system_type = 1 ;(0=Electric) [GeneralEngineData] engine_type = 1 ;1=Jet Engine.0 = 0,0,0 ;ZXY distance from ref datum fuel_flow_scalar = 1.0 ;Scalar for fuel flow efficiency min_throttle_limit = -0.25 ;neg for turbine reverser [TurbineEngineData] fuel_flow_gain = 0.002 ;Gain on fuel flow inlet_area = 60.0 ;Square Feet, engine nacelle inlet area rated_N2_rpm = 29920 ;RPM, 2nd stage compressor rated value static_thrust = 180000 ;Lbs, max rated static thrust at SL afterburner_available = 0 ;Afterburner available? reverser_available = 1 ;Thrust reverser available? [jet_engine] thrust_scalar = 1.0 [fuel] Center1 = 0,0,0,50000,10 ;ZXY GAL MIN fuel_type = 2 ;2 = JetA number_of_tank_selectors = 1 electric_pump = 1 [electrical] electric_always_available = 1 [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 [gear_warning_system] gear_warning_available = 0 [brakes] parking_brake = 0 ;Parking brake not available toe_brakes_scale = 0 ;Brake scalar [hydraulic_system] normal_pressure = 3000 ;PSI electric_pumps = 0 ;no electric pumps engine_map = 1,0,0,0 ;pumps on Eng1 [pitot_static] vertical_speed_time_constant = 1 pitot_heat=1.000000 ;Increasing this value will cause a more instantaneous reaction in the VSI [direction_indicators] direction_indicator.0 = 3,0 ;3=Electro-Mag Slaved Compass, 0=NA [attitude_indicators] attitude_indicator.0 = 0 ;0=None [turn_indicators] turn_indicator.0 = 1,0 ;1=Electric Gyro [stall_warning] type = 0 stick_shaker=0 [autopilot] autopilot_available = 1 flight_director_available = 0 default_vertical_speed = 700.0 autothrottle_available = 0 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 = 9.00 nav_integrator_control = 0.25 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 pitch_takeoff_ga = 8.000000 [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 [forcefeedback] ;revised to eliminate bumps 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 ;CHANGES TO AIR FILE ;-DELETE THE FOLLOWING ; 2 description ; 3 performance ; 4 registration ; 100 sim file name ; 101 normal model file name ; 300 Control Effectiveness ; 310 Engine Type ; 311 number of engines ; 312 Fuel Weight per Gallon ; 313 Reverse Thrust ; 314 Land Me ; 315 flaps positions ; 316 Max Operating Mach Mmo ; 317 Autopilot Settings ; 318 flaps available ; 319 Aural Stall Warning ; 322 Mixture Control Available ; 323 Carb Ht Available ; 324 Pitot Heat available ; 325 gear warning ; 327 spoiler available ; 328 is taildragger ; 329 Speed Hold Switches ; 330 Prop Type ; 331 Strobe Lights ; 332 Wheel Brakes ; 333 OBS Available ; 334 Gyro Drift ; 335 Avionics ; 337 spoiler deploy available ; 338 Autobrake ; 339 stick shaker ; 340 spoilerons ; 344 Smoke ; 516 Aileron and Rudder trim ; 517 Elevator Deflection ; 518 Aileron Deflection ; 519 Rudder Deflection ;1001 Moment of Inertia values ;1002 Engine Locations ;1202 Autopilot trim ;1520 Fuel System ;1533 Flight Director ;1534 Wing Centre of Lift ;-CHANGE THE FOLLOWING ; 1 aircraft name from Boeing 747-400 to Liberty Ship (based on 4-engine jet template) ; 320 control surfaces ; flap angle limit from .698 to 0 ; spoiler angle limit from .7854 to 0 ;1101 primary aerodynamics ;--Misc ; empty weight from 535000 to 401100 ;--Drag ; drag coefficient - zero lift * 2048 from 31 to 32767 ; skin friction coefficient? *-65536 from -73 to -32768 ; all the rest to "0" ;--Lift ; lift - flaps from 1.8 to 0 ; lift - spoilers from .48 to 0 ;--Pitch ; pitch moment - flaps from .0105 to 0 ; pitch moment - gear from .0171 to 0 ; pitch moment - spoilers from -.01 to 0 ;1501 engine fs2000 turbine ; thrust - change from 56750 to 180000 [vacuum_system] max_pressure=5.150000 vacuum_type=2 electric_backup_pressure=0.000000 engine_map=0,0,0,0 [pneumatic_system] max_pressure=18.000000 bleed_air_scalar=1.000000 [deice_system] structural_deice_type=0
