//+------------------------------------------------------------------+
//|                              Mig-29 K                            |
//|                             version  6                           |
//|                           2003 fev. 14                           |
//+------------------------------------------------------------------+

[fltsim.0]
title=Mig-29K Paint1
sim=Mig-29K
model=
panel=
sound=
texture=1
kb_checklists=Mig-29K_check
kb_reference=Mig-29K_ref
description=Hauteur : 4.73 m\nLongueur : 17.32 m\nEnvergure : 11.36 m\nMasse maxi au dйcollage : 18 500 kg\nModelisй par Barneybigard 02/2003\nModиle de vol Benoit Dubй et Sonny
ui_manufacturer=Mig
ui_type=29K
ui_variation=Version navale

[General]
performance=Weight: empty 24,416000                                     Speed: 1,033 kt                                                   Thrust: 15,785 w\/afterburning                              \n\n

//0  Classe
//1  Position longitudinale       (pieds)
//2  Position latйrale            (pieds)
//3  Position verticale           (pieds)
//4  Seuil dommage impact         (pieds/minute)
//5  Freins                       (0=aucun, 1=Gauche, 2=Droit)
//6  Rayon roues                  (pieds)
//7  angle braquage               (degrйs)
//8  Compression statiqu          (pieds) (0 si rigide)
//9  Ratio compression statique/max
//10 Ratio amortissement          (0=non amortie, 1=amortissement critique)
//11 Temps de sortie train        (secondes)
//12 Temps rentrйe train          (secondes)
//13 Sound Type
//14 vitesse max rentrйe train    (kias)
//15 vitesse max endomage train   (kias)

[contact_points]
// Train      0          1           2           3           4          5         6         7        8           9        10       11          12         13         14          15   
point.0=  1.000000, 7.85905512, 0.00000000,  -9.5500 , 2762.204800, 0.000000, 3.570591, 30.0000, 1.08000000, 1.220000,  1.00 ,  7.000000,  8.000000,  0.000000,  200.000000, 200.000000
point.1=  1.000000,-9.0488189, -6.79291339,  -8.8500,  2762.204800, 1.000000, 4.570591,  0.0000, 0.52000000, 0.750000,  1.00 ,  7.000000,  8.000000,  2.000000,  200.000000, 200.000000
point.2=  1.000000,-9.0488189,  6.79291339,  -8.8500,  2762.204800, 2.000000, 4.570591,  0.0000, 0.52000000, 0.750000,  1.00 ,  7.000000,  8.000000,  3.000000,  200.000000, 200.000000
// points de contact         2       3       4        5      6      7      8      9     10      11     12     13     14     15
point.3= 2.000, -12.333, -13.333, -0.750, 1574.803, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 5.000, 0.000, 0.000
point.4= 2.000, -12.333,  13.333, -0.750, 1574.803, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 6.000, 0.000, 0.000
point.5= 2.000, -26.167,   0.000,  0.833, 1574.803, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 9.000, 0.000, 0.000
point.6= 2.000,  17.083,   0.000, -1.917, 1574.803, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 4.000, 0.000, 0.000

static_pitch=-1.038208
static_cg_height=8.735757

[WEIGHT_AND_BALANCE]
reference_datum_position=0.000000,0.000000,0.000000
empty_weight_CG_position=0.000000,0.000000,0.000000
max_number_of_stations=50
station_load.0=0.000000,0.000000,0.000000,0.000000
empty_weight=24000.000000                             // (livres) masse а vide
empty_weight_roll_MOI=69000.000000                    // moment d'inertie roulis
empty_weight_pitch_MOI=116000.000000                  // moment d'inertie tangage
empty_weight_yaw_MOI=172600.000000                    // moment d'inertie lacet
empty_weight_coupled_MOI=1200.000000                  // moment d'inertie couplй

[fuel]
//--------Av./Arr.--gau./droit----vert.------Capacite-------Non util--
//         pieds      pieds      pieds       gallons       gallons
LeftMain=0.000000,-5.000000,0.000000,710.000000,0.000000
LeftAux=0.000000,-3.333333,0.000000,370.000000,0.000000
RightMain=0.000000,5.000000,0.000000,710.000000,0.000000
RightAux=0.000000,3.333333,0.000000,370.000000,0.000000
fuel_type=2.000000
number_of_tank_selectors=1

[airplane_geometry]
                                       // Ailes
                                       // -----
wing_area=379.000000                   // (pieds carrйs) surface ailaire
wing_span=37.250000                    // (pieds) envergure
wing_root_chord=13.083333              // (pieds) corde а l'emplanture
wing_dihedral=0.000000                 // (degrйs) diиdre
wing_incidence=0.0000                  // (degrйs) incidence а l'emplanture
wing_twist=0.000000                    // (degrйs) vrillage
oswald_efficiency_factor=5.189367      // mesure de l'efficacitй de la portance de l'aile
wing_winglets_flag=0                   // ailerettes disponibles? 0=non, 1=oui
wing_sweep=0.000000                    // (degrйs) flиche
wing_pos_apex_lon=0.000000             // (pieds)
wing_pos_apex_vert=0.000000            // (piedsw)
                                       // stablisateur
                                       // -------------
htail_area=176.000000                  // (pieds carrйs) surface stabilisateur
htail_span=25.416667                   // (pieds) envergure stabilisateur
htail_pos_lon=-21.750000               // (pieds) position longi. stabilisateur
htail_pos_vert=0.000000                // (pieds) position vet. stabilisateur
htail_incidence=0.000000               // (degrйs) incidence stabilisateur
htail_sweep=0.000000                   // (degrйs) flиche
                                       // Dйrive
                                       // ------
vtail_area=176.000000                  // (pieds carrйs) surface dйrive
vtail_span=15.126136                   // (pieds) hauteur dйrive
vtail_sweep=0.000000                   // (pieds) flиche dйrive
vtail_pos_lon=-20.750000               // (pieds) position longi. dйrive
vtail_pos_vert=8.500000                // (pieds) position vert. dйrive
                                       // surfaces des gouvernes
                                       // ---------------------- 
elevator_area=40.000000                // (pieds carrйs) gouverneprofondeur
aileron_area=25.000000                 // (pieds carrйs) ailerons
rudder_area=16.490000                  // (pieds carrйs) gouverne direction
elevator_up_limit=27.501974            // (degrйs) limite sup. profondeur
elevator_down_limit=20.626481          // (degrйs) limite inf. profondeur
aileron_up_limit=19.480565             // (degrйs) limite sup. aileron
aileron_down_limit=19.480565           // (degrйs) limite inf. aileron
rudder_limit=23.491270                 // (degrйs) limite gouv. direction
elevator_trim_limit=19.480565          // (degrйs) limite compensateur profondeur
spoiler_limit=59.988681                // (degrйs) limite aйrofreins
spoilerons_available=0                 // aileron aйrofrein disponible? 0=non, 1=oui
aileron_to_spoileron_gain=0.000000     // gain aileon - aйrofrein
min_ailerons_for_spoilerons=0.000000   // (degrйs)
min_flaps_for_spoilerons=0.000000      // position min. volets pour action aileron aйrofrein

[Flaps.0]
type=1                                  // 1=bord de fuite, 2=bord d'attaque
span-outboard=0.500000                  // 0.0, ..., 1.0
extending-time=3.000000                 // (secondes)
system_type=0
flaps-position.0=0.000000,0.000000      // (degrйs)
flaps-position.1=11.996227,0.000000     // (degrйs)
flaps-position.2=31.992454,0.000000     // (degrйs)

[GeneralEngineData]
engine_type=1                           // 0=Piston, 1=Jet, 2=Aucun, 3=Helo-Turbine, 4=Fusйe, 5=Turboprop
Engine.0=-2.333333,-3.416667,0.000000   // (pieds) position moteur 1 longitudinale, latйrale, verticale par rapport au point ref.
Engine.1=-2.333333,3.416667,0.000000    // (pieds) position moteur 2 longitudinale, latйrale, verticale par rapport au point ref.
fuel_flow_scalar=1.000000               // scalaire pour efficacitй dйbit carburant

[TurbineEngineData]
fuel_flow_gain=0.002400                 // Gaim dйbit carburant
inlet_area=8.000000                     // (pieds carrйs) surface entrйe air
rated_N2_rpm=29920.000000               // (tours/minute) valeur nominale vit. rotation 2-иme йtage compresseur
static_thrust=18300.000000              // (livres) poussйe nominale statique max au niveau de la mer
afterburner_available=1                 // rйchauffe disponible? 0=non, 1=oui
reverser_available=1                    // inverseur poussйe disponible? 0=non, 1=oui

[flight_tuning]
cruise_lift_scalar     = 0.7
parasite_drag_scalar   = 1.0
induced_drag_scalar    = 1.0
elevator_effectiveness = 0.8		    // Gouvernes de profondeur Efficacitй maxi 1.0
aileron_effectiveness  = 0.8		    // Ailerons Efficacitй maxi 1.0
rudder_effectiveness   = 0.8		    // Gouvernes de direction Efficacitй maxi 1.0
pitch_stability        = 1.0
roll_stability         = 1.0
yaw_stability          = 1.0
elevator_trim_effectiveness = 1.0
aileron_trim_effectiveness  = 1.0
rudder_trim_effectiveness   = 1.0

[Reference Speeds]
flaps_up_stall_speed=122.000000          // (noeuds) vitesse vraie
full_flaps_stall_speed=97.600000         // (noeuds) vitesse vraie
cruise_speed=1302.555112                 // (noeuds) vitesse vraie

[keyboard_response]
elevator=150.000000,250.000000
aileron=150.000000,250.000000
rudder=150.000000,250.000000

[Views]
eyepoint=10.0,0.000000,-1.0

[autopilot]
autopilot_available=1
flight_director_available=0
default_vertical_speed=1800.000000
autothrottle_available=1
autothrottle_arming_required=0
autothrottle_takeoff_ga=0
autothrottle_max_rpm=90.000000
pitch_takeoff_ga=8.000000
[direction_indicators]
direction_indicator.0=3,0

[EFFECTS]
wake=fx_wake
water=fx_spray
dirt=fx_tchdrt
concrete=fx_sparks
touchdown=fx_tchdwn_s, 1
touchdown=fx_tiremark_8, 1           //-----------ajoute des petites traces de pneus

[SMOKESYSTEM]
/////////// After-Burner ///////////////////
smoke.0=0.0, -21.0, -2.70, fx_MIG29_Burner1
smoke.1=0.0, -21.0,  2.70, fx_MIG29_Burner2
smoke.2=0.0, -10.0, -3.20, fx_MIG29_Jetsmoke
smoke.3=0.0, -10.0,  3.20, fx_MIG29_Jetsmoke

[LIGHTS]
light.0=4,   12.600,   0.00,  0.600, fx_vclighth
light.1=4,   12.600,   0.00,  1.400, fx_vclighth
/////////////// wingtip vortex ////////////////////////---uses strobe lights
light.2=2,  -12.30,  -18.70,  -2.55,   fx_MIG29_Wingtip
light.3=2,  -12.30,   18.70,  -2.55,   fx_MIG29_Wingtip
/////////////// flaptip vortex ////////////////////////---uses logo lights
light.4=9,  -11.20,  -11.0,   -2.85,   fx_MIG29_Flaptip
light.5=9,  -11.20,   11.0,   -2.85,   fx_MIG29_Flaptip
/////////////// strake vortex /////////////////////////---uses taxi lights
light.6=6,    5.0,    -3.6,   -0.60,   fx_MIG29_Strake
light.7=6,    5.0,     3.6,   -0.60,   fx_MIG29_Strake  
///////////////////////////////////////////////////////

[forcefeedback]
stick_shaker_magnitude=1000             ; 0 - 10000
stick_shaker_direction=0                ; 0 - 35999 degrees
stick_shaker_period=111111              ; in microseconds
gear_bump_nose_magnitude=6000           ; 0 - 10000
gear_bump_nose_direction=18000          ; 0 - 35999 degrees
gear_bump_nose_duration=250000          ; in microseconds
gear_bump_left_magnitude=6000           ; 0 - 10000
gear_bump_left_direction=35500          ; 0 - 35999 degrees
gear_bump_left_duration=250000          ; in microseconds
gear_bump_right_magnitude=6000          ; 0 - 10000
gear_bump_right_direction=00500         ; 0 - 35999 degrees
gear_bump_right_duration=250000         ; in microseconds
ground_bumps_magnitude1=3250            ; 0 - 10000
ground_bumps_angle1=8900                ; 0 - 35999 degrees
ground_bumps_intercept1=5.0
ground_bumps_slope1=0.48
ground_bumps_magnitude2=750             ; 0 - 10000
ground_bumps_angle2=9100                ; 0 - 35999 degrees
ground_bumps_intercept2=0.075
ground_bumps_slope2=1.0

[TailHook]
tailhook_length=5.30                           ;(feet)
tailhook_position=-18.50, 0.0, -3.50           ;(feet) longitudinal, lateral, vertical positions from datum
cable_force_adjust=1.0

[folding_wings]
wing_fold_system_type = 4                     ;0=None
fold_rates = 0.12,0.11                        ;Percent per second