Su-26M Просмотр ZIP-архива

SU-26M/Aircraft.cfg

[fltsim.0]
title=SU-26M
sim=SU26M
model=
panel=
sound=
texture=
kb_checklists=
kb_reference=
atc_id_color=0000000000
atc_id=SU-26M
ui_manufacturer=Sukhoi
ui_type=SU-26M
ui_variation=Бело-синий
description=Одноместный спортивно-пилотажный самолет Су-26М создан в ОКБ им. П.О. Сухого для выполнения наиболее сложных комплексов фигур высшего пилотажа, является одним из лучших в мире самолетов для обучения, тренировки и участия летчиков в соревнованиях по высшему пилотажу и показательных выступлениях. \nС 1986 года на самолете завоевано более ста пятидесяти медалей на чемпионатах мира и Европы, из них более девяноста золотых. В 1992-93 годах на самолетах Су-26М выиграны национальные первенства США и Австралии. \nБлагодаря своей уникальной конструкции, изготовленной на основе новейших технологий, самолет не уступает, появившимся значительно позже, лучшим зарубежным спортивно-пилотажным самолетам, а сочетание характеристик максимальной допустимой перегрузки, угловой скорости крена и скороподъемности все еще остается непревзойденным. \n
atc_heavy=0
atc_airline=
atc_flight_number=
visual_damage=1

[General]
atc_type=SU-26M 
atc_model= 
editable=1 
performance=Максимально допустимая скорость полета, км\/ч   450\nМаксимальная скорость горизонтального полета, км\/ч 310\nДальность полета, км 895\nПосадочная скорость, км\/ч 130\nВзлетная скорость, км\/ч 130\nВзлетная масса в пилотажном варианте, кг 790\nДвигатель, Мощность, л.с. 360\nПрактический потолок, м 4000 
 
 
 
 
Максимальная скорость горизонтального полета, км/ч 310  
Дальность полета, км 895 
Посадочная скорость, км/ч 130
Взлетная скорость, км/ч 130
Взлетная масса в пилотажном варианте, кг 790  
Двигатель, Мощность, л.с. 360
Практический потолок, м 4000
 

[weight_and_balance]

// ACM V2.3
max_gross_weight = 1840
empty_weight = 1500
reference_datum_position = 0, 0, 0
empty_weight_CG_position = -1.6, 0, 0
empty_weight_pitch_MOI = 1077
empty_weight_roll_MOI = 748
empty_weight_yaw_MOI = 500
empty_weight_coupled_MOI = 0
max_number_of_stations = 1

station_load.0 = 170, -4.42, 0, 0.70

CG_forward_limit=0.000
CG_aft_limit=1.000

[lights]

//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing

light.0 = 3, 0, -12.5, -0.37, fx_navred
light.1 = 3, 0, 12.5, -0.38, fx_navgre
light.2 = 2, -0.3, -12.5, -0.4, fx_strobe
light.3 = 2, -0.3, 12.5, -0.38, fx_strobe
light.4 = 4, -6.06, 0, 0.80, fx_vclight

[GeneralEngineData]

//0=Piston, 1=Jet, 2=None, 3=Helo-Turbine, 4=Rocket, 5=Turboprop
engine_type = 0
fuel_flow_scalar = 1.000
engine.0 = 5.25, 0, 0,
min_throttle_limit=0.000000

[smokesystem]
smoke.0 = 0.01, -3.00, 0, fx_smoke_w

[effects]
wake = fx_wake
water = fx_spray
dirt = fx_tchdrt
concrete = fx_sparks
touchdown = fx_tchdwn_s, 1

[fuel]

//Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)

fuel_type = 1
number_of_tank_selectors = 1

Center1 = -2.6, 0, 0, 15.85, 0
electric_pump=0


[contact_points]
static_pitch = 13
static_cg_height = 4.5
max_number_of_points = 9

point.0 = 1, -14.7652, 0, -1.7338, 1600, 0, 0.656166, 34.08, 0.3, 0.8, 0.7, 0, 0, 0, 0, 0
point.1 = 1, 0.7428, -4, -5.05, 3500, 1, 1.3123, 0, 0.8, 1.5, 0.912718, 0, 0, 2, 0, 0
point.2 = 1, 0.7702, 4, -5.05, 3500, 2, 1.3123, 0, 0.8, 1.5, 0.912718, 0, 0, 3, 0, 0
point.3 = 2, 0, -12.7, -0.5, 1574.80315, 0, 0, 0, 0, 0, 0, 0, 0, 5, 0, 0
point.4 = 2, 0, 12.7, -0.5, 1574.80315, 0, 0, 0, 0, 0, 0, 0, 0, 6, 0, 0
point.5 = 2, -15.7322, 0, -0.0885, 1574.80315, 0, 0, 0, 0, 0, 0, 0, 0, 9, 0, 0
point.6 = 2, 3.4625, 0, -1.7973, 1574.80315, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0
point.7 = 2, -14.5128, 0, 3.966, 1574.80315, 0, 0, 0, 0, 0, 0, 0, 0, 7, 0, 0
point.8 = 2, -2.8814, 0, -1.3807, 1574.80315, 0, 0, 0, 0, 0, 0, 0, 0, 8, 0, 0


[keyboard_response]
elevator = 140, 240
aileron = 200, 1000
rudder = 200, 1000


[forcefeedback]
ground_bumps_magnitude1 = 3000
ground_bumps_angle1 = 8900
ground_bumps_intercept1 = 4.0
ground_bumps_slope1 = 0.25
ground_bumps_magnitude2 = 350
ground_bumps_angle2 = 9100
ground_bumps_intercept2 = 0.075
ground_bumps_slope2 = 0.7
crash_magnitude1 = 10000
crash_direction1 = 01000
crash_magnitude2 = 10000
crash_direction2 = 9000
crash_period2 = 75000
crash_duration2 = 2500000
stick_shaker_magnitude = 500
stick_shaker_direction = 500
stick_shaker_period = 111111

[airplane_geometry]
//ACM_AREAW1// 0.3824,0.3824,0.0274,2.2195,0.6097,0.6097,0.0348,1.8997,0.8590,0.8590
//ACM_AREAW2// 0.0450,1.7948,1.2884,1.2884,0.0675,1.7201,1.7180,1.7180,0.0900,1.6454
//ACM_AREAW3// 2.1479,2.1479,0.1124,1.5707,2.5775,2.5775,0.1350,1.4960,3.0071,3.0071
//ACM_AREAW4// 0.1576,1.4213,3.4367,3.4367,0.1800,1.3466,3.8210,3.8210,0.2026,1.2869
//ACM_AREAH1// 0.0996,0.0996,0.0274,0.7541,0.2088,0.2088,0.0373,1.0678,0.2610,0.2610
//ACM_AREAH2// 0.0467,1.0607,0.5018,0.5018,0.0688,1.0225,0.6740,0.6740,0.0834,0.9965
//ACM_AREAH3// 0.8388,0.8388,0.1030,0.9707,0.9858,0.9858,0.1176,0.9502,1.2265,1.2265
//ACM_AREAH4// 0.1473,0.9168,1.3255,1.3255,0.1641,0.8985,1.4270,1.4270,0.1888,0.8830
//ACM_AREAV1// -0.6485,-0.6485,0.6941,1.0189,-0.6110,-0.6110,0.6973,1.4155,-0.3355,-0.3355
//ACM_AREAV2// 0.6930,1.3394,-0.0719,-0.0719,0.6983,1.2610,0.0063,0.0063,0.0115,1.2374
//ACM_AREAV3// 0.3587,0.3587,0.2116,1.1397,0.4781,0.4781,0.2770,1.0994,0.5590,0.5590
//ACM_AREAV4// 0.3231,1.0784,0.6520,0.6520,0.3693,1.0477,0.7498,0.7498,0.4156,1.0196
//ACM_CAREAW1// 1.1641,1.1641,1.3235,1.7451,2.1229,2.1229,1.1576,1.5793,2.3589,2.3589
//ACM_CAREAW2// 1.1188,1.5384,2.5659,2.5659,1.0785,1.5010,2.7808,2.7808,1.0417,1.4643
//ACM_CAREAW3// 3.0051,3.0051,1.0030,1.4270,3.1930,3.1930,0.9700,1.3918,3.4098,3.4098
//ACM_CAREAW4// 0.9312,1.3530,3.5766,3.5766,0.9060,1.3257,3.8394,3.8394,0.8575,1.2773
//ACM_CAREAH1// 0.1036,0.1036,0.4990,0.7562,0.2122,0.2122,0.4986,1.0635,0.4104,0.4104
//ACM_CAREAH2// 0.5030,1.0377,0.5691,0.5691,0.5012,1.0161,0.7329,0.7329,0.5016,0.9886
//ACM_CAREAH3// 0.9214,0.9214,0.4981,0.9613,1.0426,1.0426,0.4986,0.9434,1.2580,1.2580
//ACM_CAREAH4// 0.4970,0.9103,1.2582,1.2582,0.1611,0.9096,1.4349,1.4349,0.1903,0.8901
//ACM_CAREAV1// -0.6463,-0.6463,0.7013,1.0188,-0.6205,-0.6205,0.7020,1.4170,-0.2946,-0.2946
//ACM_CAREAV2// 0.7026,1.3299,0.0648,0.0648,0.7006,1.2235,0.3355,0.3355,0.6963,1.1411
//ACM_CAREAV3// 0.5630,0.5630,0.6970,1.0756,0.5644,0.5644,0.3226,1.0772,0.6503,0.6503
//ACM_CAREAV4// 0.3664,1.0528,0.7095,0.7095,0.4149,1.0353,0.7570,0.7570,0.5691,1.0226
wing_area = 112.000
wing_span = 25.37
wing_root_chord = 6.25
wing_dihedral = 0
wing_incidence = 0.000
wing_twist = 0.000
oswald_efficiency_factor = 0.600
wing_winglets_flag = 0
wing_sweep = 3
wing_pos_apex_lon = 1.28
wing_pos_apex_vert = -0.38
htail_area = 28.000
htail_span = 9.43
htail_pos_lon = -11.27
htail_pos_vert = 1.29
htail_incidence = 0.000
htail_sweep = 7
vtail_area = 15
vtail_span = 2.46
vtail_sweep = 29
vtail_pos_lon = -11.17
vtail_pos_vert = 1.55
elevator_area = 10.000
aileron_area = 18.400
rudder_area = 7.000
elevator_up_limit = 25.000
elevator_down_limit = 25.000
aileron_up_limit = 25.000
aileron_down_limit = 25.000
rudder_limit = 32.000
elevator_trim_limit = 25.000
spoiler_limit = 0.000
aileron_to_spoileron_gain = 0.000
min_ailerons_for_spoilerons = 0.000
min_flaps_for_spoilerons = 0.000
spoilerons_available = 0

[electrical]
max_battery_voltage = 12
generator_alternator_voltage = 27
max_generator_alternator_amps = 40
electric_always_available = 0
avionics_bus = 0, 5, 9.5
avionics = 1, 5, 9.5
additional_system = 0, 2, 9.5
marker_beacon = 1, 2, 9
fuel_pump = 0, 5, 9

[flight_tuning]
cruise_lift_scalar=1.000 
parasite_drag_scalar=1.000 
induced_drag_scalar=1.000 
elevator_effectiveness=1.000 
aileron_effectiveness=1.000 
rudder_effectiveness=1.000 
pitch_stability=1.000 
roll_stability=1.000 
yaw_stability=1.000 
elevator_trim_effectiveness=1.000 
aileron_trim_effectiveness=1.000 
rudder_trim_effectiveness=1.000 
hi_alpha_on_roll=-0.323
hi_alpha_on_yaw=0.16
p_factor_on_yaw=0.521
torque_on_roll=0.3
gyro_precession_on_yaw=0.3
gyro_precession_on_pitch=0.3

[piston_engine]
power_scalar=1.000 
cylinder_displacement=90.300 
compression_ratio=8.700 
number_of_cylinders=9 
max_rated_rpm=2700.000 
max_rated_hp=300.000 
fuel_metering_type=0 
cooling_type=0 
normalized_starter_torque=0.300 
turbocharged=0 
max_design_mp=0.000 
min_design_mp=0.000 
critical_altitude=0.000 
emergency_boost_type=0 
emergency_boost_mp_offset=0.000 
emergency_boost_gain_offset=0.000 
fuel_air_auto_mixture=0 
auto_ignition=0 
max_rpm_mechanical_efficiency_scalar=1.000 
idle_rpm_mechanical_efficiency_scalar=1.000 
max_rpm_friction_scalar=1.000 
idle_rpm_friction_scalar=1.000 

[propeller]
thrust_scalar=1.000 
propeller_type=0 
propeller_diameter=7.874 
propeller_blades=2 
propeller_moi=5.900 
beta_max=34.000 
beta_min=17.000 
min_gov_rpm=1400.000 
prop_tc=0.100 
gear_reduction_ratio=1.000 
fixed_pitch_beta=0.000 
low_speed_theory_limit=80.000 
prop_sync_available=0 
prop_deice_available=0 
prop_feathering_available=0 
prop_auto_feathering_available=0 
min_rpm_for_feather=0.000 
beta_feather=0.000 
power_absorbed_cf=0.000 
defeathering_accumulators_available=0 
prop_reverse_available=0.000 
minimum_on_ground_beta=0.000 
minimum_reverse_beta=0.000 
        //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

[brakes]
parking_brake = 1       //Parking brake available
toe_brakes_scale = 0.6  //Brake scalar
differential_braking_scale = 0.0        //Delta on the amount of brake when the rudder pedals deflected
[hydraulic_system]
normal_pressure = 0.0    //PSI        
[Views]
eyepoint=-6.00, 0.00, 1.80 

[Radios]
// Radio Type = availiable, standby frequency, has glide slope
Audio.1=1 
Com.1=1, 1 
Nav.1=1, 1, 1 
Adf.1=1 
Transponder.1=1 
Marker.1=1 

[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=1,0 

[attitude_indicators]
//Type: 0=None, 1=Vacuum Gyro, 2=Electric Gyro
attitude_indicator.0 = 1 
[turn_indicators]
//Type: 0=None, 1=Electric Gyro, 2=Vacuum Gyro
turn_indicator.0=1,0
[Reference Speeds]
//flaps_up_stall_speed=55.000 
//full_flaps_stall_speed=55.000 
cruise_speed=167.387 
max_indicated_speed     = 243                   //Red line (KIAS)
flaps_up_stall_speed=55.000 
full_flaps_stall_speed=44.000 

[autopilot]
autopilot_available=0 
flight_director_available=0 

[stall_warning]
type=2
[gear_warning_system]
gear_warning_available=0
pct_throttle_limit=0.000000
flap_limit_power=0.000000
flap_limit_idle=0.000000
[Flaps.0]
type= 0
span-outboard= 0.125
extending-time= 5.000
system_type= 4
damaging-speed= 0.000
blowout-speed= 0.000
lift_scalar= 1.000
drag_scalar= 1.000
pitch_scalar= 1.000

SU-26M.zip

Имя файла Дата Размер
SU-26M/ 20.06.2005 18:34
SU-26M/Aircraft.cfg 19.06.2005 00:43 11 KB
SU-26M/Su26M.air 19.06.2005 00:14 10 KB
SU-26M/SU.jpg 20.06.2005 17:46 177 KB
SU-26M/version.txt 20.06.2005 17:57 9 B
SU-26M/dev_note.txt 20.06.2005 18:32 641 B
SU-26M/license_info.txt 21.06.2005 12:44 1 KB
SU-26M/Gauges/ 20.06.2005 18:34
SU-26M/Gauges/SU-26.CAB 15.05.2005 13:49 425 KB
SU-26M/TEXTURE/ 20.06.2005 18:34
SU-26M/TEXTURE/prop_spinner_T.bmp 13.06.2005 00:11 16 KB
SU-26M/TEXTURE/Fuselage_T.bmp 09.06.2005 03:00 1 MB
SU-26M/TEXTURE/Any_T.bmp 09.05.2005 00:59 64 KB
SU-26M/TEXTURE/Wings_T.bmp 18.06.2005 22:31 1 MB
SU-26M/TEXTURE/$_L.bmp 19.04.2005 12:57 256 KB
SU-26M/TEXTURE/$_R.bmp 19.04.2005 12:57 256 KB
SU-26M/TEXTURE/Cabin_in_T.bmp 09.04.2005 15:17 256 KB
SU-26M/TEXTURE/Kreslo.bmp 21.04.2005 02:26 64 KB
SU-26M/TEXTURE/prop_backA_T.bmp 05.05.2005 04:06 64 KB
SU-26M/TEXTURE/prop_backB_T.bmp 05.05.2005 04:06 64 KB
SU-26M/TEXTURE/prop_frontA_T.bmp 05.05.2005 05:18 64 KB
SU-26M/TEXTURE/prop_frontB_T.bmp 05.05.2005 05:46 64 KB
SU-26M/TEXTURE/Panel_Ext.bmp 18.06.2005 23:24 512 KB
SU-26M/SOUND/ 20.06.2005 18:34
SU-26M/SOUND/canopy_latch_close.wav 10.04.2003 04:06 96 KB
SU-26M/SOUND/canopy_latch_open.wav 10.04.2003 04:06 85 KB
SU-26M/SOUND/ee1a.wav 18.04.2001 10:20 55 KB
SU-26M/SOUND/ee1b.wav 18.04.2001 10:20 36 KB
SU-26M/SOUND/ee2a.wav 18.04.2001 10:20 44 KB
SU-26M/SOUND/ee2b.wav 18.04.2001 10:20 42 KB
SU-26M/SOUND/ee3a.wav 18.04.2001 10:20 20 KB
SU-26M/SOUND/ee4a.wav 18.04.2001 10:20 44 KB
SU-26M/SOUND/eep1a.wav 18.04.2001 10:20 58 KB
SU-26M/SOUND/eep1b.wav 18.04.2001 10:20 59 KB
SU-26M/SOUND/eep2a.wav 18.04.2001 10:20 67 KB
SU-26M/SOUND/eep2b.wav 18.04.2001 10:20 59 KB
SU-26M/SOUND/eeshuta.wav 18.04.2001 10:20 32 KB
SU-26M/SOUND/eeshutb.wav 18.04.2001 10:20 36 KB
SU-26M/SOUND/eestarta.wav 18.04.2001 10:20 9 KB
SU-26M/SOUND/eestartb.wav 18.04.2001 10:20 35 KB
SU-26M/SOUND/ewind.wav 18.04.2001 10:20 29 KB
SU-26M/SOUND/sound.cfg 10.04.2003 04:06 7 KB
SU-26M/SOUND/xee1a.wav 18.04.2001 10:20 54 KB
SU-26M/SOUND/xee1b.wav 18.04.2001 10:20 38 KB
SU-26M/SOUND/xee2a.wav 18.04.2001 10:20 49 KB
SU-26M/SOUND/xee2b.wav 18.04.2001 10:20 49 KB
SU-26M/SOUND/xee3a.wav 18.04.2001 10:20 29 KB
SU-26M/SOUND/xee4a.wav 18.04.2001 10:20 41 KB
SU-26M/SOUND/xeep1a.wav 18.04.2001 10:20 58 KB
SU-26M/SOUND/xeep1b.wav 18.04.2001 10:20 59 KB
SU-26M/SOUND/xeep2a.wav 18.04.2001 10:20 67 KB
SU-26M/SOUND/xeep2b.wav 18.04.2001 10:20 59 KB
SU-26M/SOUND/xeeshuta.wav 18.04.2001 10:20 25 KB
SU-26M/SOUND/xeeshutb.wav 18.04.2001 10:20 26 KB
SU-26M/SOUND/xeestarta.wav 18.04.2001 10:20 5 KB
SU-26M/SOUND/xeestartb.wav 18.04.2001 10:20 30 KB
SU-26M/PANEL/ 20.06.2005 18:34
SU-26M/PANEL/panel.cfg 13.06.2005 00:52 2 KB
SU-26M/PANEL/Su26M_1024.bmp 06.04.2005 00:22 5 MB
SU-26M/MODEL/ 20.06.2005 18:34
SU-26M/MODEL/model.cfg 09.02.2005 23:25 24 B
SU-26M/MODEL/Su26M.mdl 18.06.2005 23:10 2 MB
avsim_ru.diz 21.06.2005 18:23 381 B
Итого: 13 MB
Su-26M | Rating: 4.7!
Model of aerobatic aeroplane Su-26M
→ Size: 4 MB
→ Date: 21 years ago (21.06.2005 13:22)
→ Author:
→ License: Freeware - Free version, Do Not Redistribute
→ Downloaded: 4511 time(s)