;Cimmeron Fleet Oiler ;By Earl Watkins [fltsim.0] title=USS MISPILLION AO-105 sim=FSDS object model= panel= sound= texture= kb_checklists=mispillion_check kb_reference=mispillion_ref atc_id= ui_manufacturer=Skip's Drydock ui_type=Cimmeron Fleet Oiler ui_variation=AO-105 description=Beginning early in the 20th Century, Fleet Oilers played a crucial part in providing fuel oil to U.S. Naval ships deployed far from home. USS Mispillion AO-105 was one of many to provide this essential service. Commissioned 25 December 1945, Mispillion served with distinction throughout her career, taking part in numerous conflicts around the world. Originally built to carry 95,000 barrels of fuel oil, in 1965 she went through an extensive overhaul period, expanding her capacity to 188,095 barrels. This transformation was often referred to as "Jumboization". The model depicted here, is as she appeared in the early 1970's. A unique feature is the "Union 76" orange ball which rotates, and is illuminated at night. This feature is as it was in real life at that time. Ships making their approach for underway replenishment could clearly see the "ball". atc_airline=US Navy atc_heavy=0 atc_flight_number= [General] atc_type= atc_model= editable=1 performance=Maximum Speed\t20 kts\nCruise Speed\t11 kts\nMaximum Range\t19,000 nm\nService Ceiling\t0 ft\nFuel Capacity\t12,500 barrels\nMax Gross Weight\t20 million lbs\nSeating\t\t81\nUseful Load\t18 million lbs\n [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,-20, -4.5, 9999, 0, 1, 05, 0.9, 8.5, 0.65, 00, 00, 2, 00, 00 point.1=4, 40, 20, -4.5, 9999, 0, 1, 05, 0.9, 8.5, 0.65, 00, 00, 3, 00, 00 point.2=4,-40,-20, -4.5, 9999, 0, 1, 00, 0.9, 8.5, 0.65, 00, 00, 2, 00, 00 point.3=4,-40, 20, -4.5, 9999, 0, 1, 00, 0.9, 8.5, 0.65, 00, 00, 3, 00, 00 point.4=1, 0, 0, -5.0, 9999, 0, 1, 00, 0.9, 8.5, 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 = 50.50, 0.00, 46.05 ;wheelhouse eyepoint = 12.50, 0.00, 43.25 ;flying deck [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, 14.18, 0.15, 42.600, fx_vclighth ;high panel/VC-lighting light.1 = 4, 14.18, 0.15, 42.600, fx_vclight ;normal panel/VC-lighting ;---external light.2 = 3, 64.000, -37.40, 35.000, fx_navred ;bridge wing left light.3 = 3, 64.000, 37.40, 35.000, fx_navgre ;bridge wing right light.4 = 3, 108.000, 0.00, 71.172, fx_navwhi ;foremast light.5 = 3, 29.500, 0.00, 84.001, fx_navwhi ;mainmast light.6 = 3, -100.000, 0.00, 72.382, fx_navwhi ;mizzenmast light.7 = 3, -328.500, 0.00, 27.800, fx_navwhi ;sternlight [EFFECTS] wake = fx_wake_l ;water = fx_spray water =fx_spray_hamagiri dirt =fx_tchdrt concrete =fx_sparks touchdown =fx_tchdwn, 1 ;[EFFECTS] ;wake = fx_wake_l, 0.0,0.0,120.6 ;water = fx_spray ;stern = fx_stern_l, 0.0,0.0,-109.3 ;Infinite = Infinite, 0.0,23.3,-2.4 [SMOKESYSTEM] ;This is enabled by gauge ;smoke.0 = 0.00,0.00,0.00,PEC_steam1_y1 ;WHITE SMOKE smoke.0 = 0.00,0.00,0.00,AO_smoke_Y1 ;BLACK SMOKE smoke.1 =68, -285.00, 28.5, fx_Drainage.fx, smoke.2 =68, -285.00, -28.5, fx_Drainage.fx, smoke.3 =68, 35.00, 38.5, fx_Drainage.fx, smoke.4 =68, 35.00, -38.5, fx_Drainage.fx, [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 [flaps.0] type = 0 [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 = 150000 ;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 ;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 [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 150000
