[fltsim.0]
title=AI Project-1123_Moskow_2004
sim=Ship_big
model=M
panel=
sound=
texture=Moskow
kb_checklists=Moskow_check
kb_reference=Moskow_ref
atc_id=108
ui_manufacturer=AI Ship
ui_type=project 1123
ui_variation=Moskow
description=Противолодочный крейсер проекта 1123 "Москва" ВМФ СССР, зав. № 701. Проект разработан ЦКБ-17 (ныне - Невское ПКБ) в г. Ленинграде в 1962 году. Построен на Черноморском судостроительном заводе в г. Николаеве. Заложен 15.12.1962, вошел в состав ВМФ 25.12.1967, списан 22.06.1995. Базировался в Севастополе и входил в состав Черноморского флота. Авиационное вооружение - 14 вертолетов (12 - Ка-25ПЛ, 1 - Ка-25ЦУ, 1 - Ка-25ПС)
atc_airline=USSR Navy
atc_heavy=0
atc_flight_number=

[fltsim.1]
title=AI Project-1123_Leningrad_2004
sim=Ship_big
model=L
panel=
sound=
texture=Leningrad
kb_checklists=Leningrad_check
kb_reference=Leningrad_ref
atc_id=109
ui_manufacturer=AI Ship
ui_type=project 1123
ui_variation=Leningrad
description=Противолодочный крейсер проекта 1123 "Ленинград" ВМФ СССР, зав. № 702. Проект разработан ЦКБ-17 (ныне - Невское ПКБ) в г. Ленинграде в 1962 году. Построен на Черноморском судостроительном заводе в г. Николаеве. Заложен 15.01.1965, вошел в состав ВМФ 22.04.1969, списан 24.06.1991.  Базировался в Севастополе и входил в состав Черноморского флота. Авиационное вооружение - 14 вертолетов (12 - Ка-25ПЛ, 1 - Ка-25ЦУ, 1 - Ка-25ПС)
atc_airline=USSR Navy
atc_heavy=0
atc_flight_number=


[General]
atc_type=
atc_model=
editable=1
performance=Maximum Speed\t28.8 kts\nCruise Speed\t19.5 kts\nMaximum Range\t9,000 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
Category=airplane


[Reference Speeds]
flaps_up_stall_speed                   = 030
full_flaps_stall_speed                 = 000
cruise_speed                           = 019
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, 140,-20, -4.5, 9999, 0, 1, 05, 0.9, 8.5, 0.65, 00, 00, 2, 00, 00
point.1=4, 140, 20, -4.5, 9999, 0, 1, 05, 0.9, 8.5, 0.65, 00, 00, 3, 00, 00
point.2=4,-140,-20, -4.5, 9999, 0, 1, 00, 0.9, 8.5, 0.65, 00, 00, 2, 00, 00
point.3=4,-140, 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
light.0 = 3,    54.000, -24.40, 61.000, fx_navredh ;левый ходовой
light.1 = 3,    54.000,  24.40, 61.000, fx_navgreh ;правый ходовой
light.2 = 3,  110.000,  0.00, 71.172, fx_navwhih   ;передний топовый
light.3 = 3,   31.500,  0.00, 89.001, fx_navwhih   ;задний топовый
light.4 = 3, -318.500,  0.30, 34.800, fx_navwhih   ;гакабортный

// -- огни судна, ограниченного в возможности маневрировать (МППСС-72)  ---
light.5 = 3, -41.00,  -31.00, 106.00, fx_navredh   ;красный
light.6 = 3, -41.00,  -31.00, 100.00, fx_navwhih   ;белый
light.7 = 3, -41.00,  -31.00, 94.00, fx_navredh   ;красный



[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
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


[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
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 150000
[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=1