Sikorsky S-42 "Clipper" Просмотр ZIP-архива

Sikorsky S-42 NC-822M/Aircraft.cfg

[fltsim.0]
title=Sikorsky S-42 NC-822M
sim=Sikorsky S-42 NC-822M
model=
panel=
sound=
texture=
kb_checklists=sikorsky_s42_check
kb_reference=sikorsky_s42_ref
ui_manufacturer=Sikorsky
ui_type=S-42 Brazilian Clipper NC-822M
ui_variation=Silver, black
prop_anim_ratio=-1.76
atc_heavy=1
atc_airline=Pan American
atc_flight_number=881
atc_id=822M
description=Four-engined flying boat. In 1935 was largest plane built in US.  Flew to both Europe and Asia with Pan Am. NC-822M was first of 10 S-42's built.

[forcefeedback]
gear_bump_nose_magnitude=6000
gear_bump_nose_direction=18000
gear_bump_nose_duration=250000
gear_bump_left_magnitude=6000
gear_bump_left_direction=35500
gear_bump_left_duration=250000
gear_bump_right_magnitude=6000
gear_bump_right_direction=500
gear_bump_right_duration=250000
ground_bumps_magnitude1=3250
ground_bumps_angle1=8900
ground_bumps_intercept1=5
ground_bumps_slope1=0.48
ground_bumps_magnitude2=750
ground_bumps_angle2=9100
ground_bumps_intercept2=0.075
ground_bumps_slope2=1
crash_magnitude1=10000
crash_direction1=1000
crash_magnitude2=10000
crash_direction2=9000
crash_period2=75000
crash_duration2=2500000
stick_shaker_magnitude=5000
stick_shaker_direction=0
stick_shaker_period=111111


[General]
performance=Maximum Speed\t183 mph\nCruise Speed\t150 mph\nRange\t\t1200 mi\nService Ceiling\t16,000 ft\nMax Gross Weight\t40,000 lb\nSeating\t\t32 passengers, 5 crew\nUseful Load\t19,076 lb\n\n
atc_type=SIKORSKY
atc_model=S42
category=airplane
editable=1

[contact_points]
//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 / Water Rudder Effectiveness  (0=Undamped, 1=Critically Damped) / 1.0 = normal
//11 Extension Time              (seconds)
//12 Retraction Time             (seconds)
//13 Sound Type
//14 Airspeed limit for retraction (KIAS)
//15 Airspeed that gear gets damage at(KIAS)

static_pitch= 2.000
static_cg_height= 7.000
gear_system_type=1
max_number_of_points=15
tailwheel_lock=0
point.0= 1, -39.000, 0.000, -8.000, 3600, 0, 1.570, 32.000, 0.300, 2.500, 0.800, 2.000, 2.000, 1
point.1= 1, 5.000, -8.000, -12.250, 3600, 1, 1.570, 0.000, 0.400, 2.500, 0.800, 2.000, 2.000, 2
point.2= 1, 5.000, 8.000, -12.250, 3600, 2, 1.570, 0.000, 0.400, 2.500, 0.800, 2.000, 2.000, 3
point.3= 2, -30.000, 0.000, -1.000, 1800, 0, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 9
point.4= 2, 18.000, 0.000, -1.500, 1800, 0, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 4
point.5= 2, -5.000, -33.500, -5.000, 1800, 0, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 5
point.6= 2, -5.000, 33.500, -5.000, 1800, 0, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 6
point.7= 4, 14.000, -4.500, -11.300, 1600, 1, 0.000, 0.000, 3.950, 1.500, 0.650, 0.000, 0.000, 2
point.8= 4, 14.000, 4.500, -11.300, 1600, 2, 0.000, 0.000, 3.950, 1.500, 0.650, 0.000, 0.000, 3
point.9= 4, -25.000, -4.500, -7.900, 1600, 0, 0.000, 30.000, 1.950, 1.500, 0.650, 0.000, 0.000, 0
point.10= 4, -25.000, 4.500, -7.900, 1600, 0, 0.000, 0.000, 1.950, 1.500, 0.650, 0.000, 0.000, 0
point.11= 5, -30.900, 0.000, -7.300, 1600, 0, 0.000, 15.000, 0.000, 0.000, 1.000, 1.000, 1.200, 0
point.12= 2, -5.000, -57.500, 10.500, 1600, 0, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 2
point.13= 2, -5.000, 57.500, 10.500, 1600, 0, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 3
point.14= 2, -59.300, 0.000, 5.000, 800, 0, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0


[WEIGHT_AND_BALANCE]
reference_datum_position= 0.000, 0.000, 0.000
empty_weight_CG_position= -2.000, 0.000, -1.000

max_number_of_stations=13

empty_weight=21945.00000
empty_weight_roll_MOI=152511.88000
empty_weight_pitch_MOI=254388.88000
empty_weight_yaw_MOI=316911.52000
empty_weight_coupled_MOI=0.00000
max_gross_weight=38000.0
CG_forward_limit= -0.860
CG_aft_limit= -2.540
station_load.0= 200, 16.400, -2.000, 0.000, Pilot
station_load.1= 200, 16.400, 2.000, 0.000, Co-Pilot
station_load.2= 200, 13.400, -2.000, 0.000, Flight
station_load.3= 200, 13.400, 2.000, 0.000, Radio
station_load.4= 1600, 10.000, 0.000, 0.000, Baggage-Mail
station_load.5= 680, 6.000, 0.000, 0.000, Passenger
station_load.6= 680, 3.000, 0.000, 0.000, Passenger
station_load.7= 680, 0.000, 0.000, 0.000, Passenger
station_load.8= 680, -3.000, 0.000, 0.000, Passenger
station_load.9= 680, -6.000, 0.000, 0.000, Passenger
station_load.10= 680, -9.000, 0.000, 0.000, Passenger
station_load.11= 680, -12.000, 0.000, 0.000, Passenger
station_load.12= 680, -15.000, 0.000, 0.000, Passenger


[fuel]
//Allowable types: Center1 Center2 Center3 LeftMain LeftAux LeftTip 
//                 RightMain RightAux RightTip External1 External2 
//LeftMain= 0.000, -8.000, 0.000, 140.000, 0.000
//LeftAux= 0.000, -17.000, 0.000, 140.000, 0.000
//LeftTip= 0.000, -20.000, 0.000, 170.000, 0.000
//RightMain= 0.000, 8.000, 0.000, 140.000, 0.000
//RightAux= 0.000, 17.000, 0.000, 140.000, 0.000
//RightTip= 0.000, 20.000, 0.000, 170.000, 0.000
//Center1= 0.000, -5.000, 0.000, 170.000, 0.000
//Center2= 0.000, 5.000, 0.000, 170.000, 0.000
LeftAux= 0.000, -17.000, 0.000, 310.000, 0.000
Center2= 0.000, -5.000, 0.000, 310.000, 0.000
Center3= 0.000, 5.000, 0.000, 310.000, 0.000
RightAux= 0.000, 17.000, 0.000, 310.000, 0.000

fuel_type=1
number_of_tank_selectors=4
electric_pump=1
fuel_dump_rate=0.02000
anemometer_pump=0
engine_driven_pump=0
manual_pump=0


[airplane_geometry]
wing_area=1330.00000
wing_span=114.00000
wing_root_chord=13.50000
wing_dihedral=3.00000
wing_incidence=0.00000
wing_twist=0.00000
oswald_efficiency_factor=0.98300
wing_winglets_flag=0
wing_sweep=0.00000
//wing_pos_apex_lon= 2.000
wing_pos_apex_lon=0.94067
wing_pos_apex_vert=3.00000
htail_area=216.00000
htail_span=35.00000
htail_pos_lon=-42.00000
htail_pos_vert=2.30000
htail_incidence=0.00000
htail_sweep=0.00000
vtail_area=145.00000
vtail_span=15.00000
vtail_sweep=16.00000
vtail_pos_lon=-42.00000
vtail_pos_vert=3.00000
elevator_area=70.00000
aileron_area=98.00000
rudder_area=72.00000
elevator_up_limit=25.00000
elevator_down_limit=25.00000
aileron_up_limit=25.00000
aileron_down_limit=12.50000
rudder_limit=24.00000
elevator_trim_limit=22.00000
spoiler_limit=0.00000
spoilerons_available=0
aileron_to_spoileron_gain=0.00000
min_ailerons_for_spoilerons=0.00000
min_flaps_for_spoilerons=0.00000
spoiler_extension_time=5.00000
spoiler_handle_available=0
auto_spoiler_available=0
positive_g_limit_flaps_up=3.70000
negative_g_limit_flaps_up=-2.96000
positive_g_limit_flaps_down=2.59000
negative_g_limit_flaps_down=-2.22000
load_safety_factor=1.00000


[GeneralEngineData]
engine_type=0
Engine.0=4.000, -18.750, 3.000
Engine.1=4.000, -6.750, 3.000
Engine.2=4.000, 6.750, 3.000
Engine.3=4.000, 18.750, 3.000
fuel_flow_scalar=1.00000
min_throttle_limit=0.04000
master_ignition_switch=1                      //Master Ignition Switch


[piston_engine]
power_scalar=1.35000
cylinder_displacement=187.78000
compression_ratio=6.00000
number_of_cylinders=9
max_rated_rpm=2300.00000
max_rated_hp=750.00000
fuel_metering_type=1
cooling_type=0
normalized_starter_torque=0.03480
turbocharged=1
max_design_mp=36.00000
min_design_mp=10.00000
critical_altitude=8000.00000
emergency_boost_type=0
emergency_boost_mp_offset=0.00000
emergency_boost_gain_offset=0.00000
fuel_air_auto_mixture=1
auto_ignition=0
max_rpm_mechanical_efficiency_scalar=1.00000
idle_rpm_mechanical_efficiency_scalar=1.00000
max_rpm_friction_scalar=1.00000
idle_rpm_friction_scalar=1.00000
emergency_boost_duration=0.00000
BestPowerSpecificFuelConsumption=0.50000
detonation_onset=46.20000


[propeller]
thrust_scalar=1.00000
propeller_type=0
propeller_diameter=11.50000
propeller_blades=3
propeller_moi=124.47758
beta_max=45.00000
beta_min=12.00000
min_gov_rpm=1400.00000
prop_tc=0.10000
gear_reduction_ratio=1.50000
fixed_pitch_beta=0.00000
low_speed_theory_limit=80.00000
prop_sync_available=1
prop_deice_available=1
prop_feathering_available=1
prop_auto_feathering_available=0
min_rpm_for_feather=700.00000
beta_feather=89.50000
power_absorbed_cf=0.90000
defeathering_accumulators_available=0
prop_reverse_available=0
minimum_on_ground_beta=0.00000
minimum_reverse_beta=0.00000
feathering_switches=1                         //Switches which invoke feathering


[Reference Speeds]
flaps_up_stall_speed=90
full_flaps_stall_speed=65
cruise_speed=160
max_indicated_speed=289.97748
max_mach=0.28000


[keyboard_response]
elevator=100.000000,140.000000
aileron=140.000000,1000.000000
rudder=140.000000,1000.000000


[Views]
eyepoint=14.50,-1.50,-0.60  //pilot seat
//eyepoint=12.50,1.50,-1.00  // radio operator
//eyepoint=12.80,0.00,-0.50  // cockpit center
//eyepoint=12.50,-2.20,-1.10  // flight engineer
//eyepoint=06.00,0.00,-2.00  // cabin 1 aisle
//eyepoint=10.50,-0.20, -2.00  //bulkhead 5
//eyepoint=-32.50,-2.00,-2.00  // cabin 2


[autopilot]
autopilot_available=1
flight_director_available=0
default_vertical_speed=700
autothrottle_available=0
pitch_takeoff_ga=8
max_pitch=10
max_pitch_acceleration=1
max_pitch_velocity_lo_alt=2
max_pitch_velocity_hi_alt=1.5
max_pitch_velocity_lo_alt_breakpoint=20000
max_pitch_velocity_hi_alt_breakpoint=28000
max_bank=25
max_bank_acceleration=1.8
max_bank_velocity=3
max_throttle_rate=0.1
nav_proportional_control=9
nav_integrator_control=0.25
nav_derivative_control=0
nav_integrator_boundary=2.5
nav_derivative_boundary=0
gs_proportional_control=9.52
gs_integrator_control=0.26
gs_derivative_control=0
gs_integrator_boundary=0.7
gs_derivative_boundary=0
yaw_damper_gain=0
default_bank_mode=2
default_pitch_mode=1
autothrottle_arming_required=0
autothrottle_takeoff_ga=1
autothrottle_max_rpm=90
use_no_default_bank=0
use_no_default_pitch=0


[direction_indicators]
direction_indicator.0=1,0


[EFFECTS]
wake=fx_wake
//water=fx_goose_spray
water=fx_spray
dirt=fx_tchdrt
concrete=fx_tchdrt
touchdown=fx_tchdwn, 1


[flight_tuning]
cruise_lift_scalar=1.00000
pitch_stability=1.00000
roll_stability=1.00000
yaw_stability=1.00000
parasite_drag_scalar=1.00000
induced_drag_scalar=1.00000
elevator_effectiveness=1.00000
aileron_effectiveness=1.00000
rudder_effectiveness=1.00000
elevator_trim_effectiveness=1.00000
aileron_trim_effectiveness=1.00000
rudder_trim_effectiveness=1.00000
hi_alpha_on_roll=1.00000
hi_alpha_on_yaw=1.00000
p_factor_on_yaw=1.00000
torque_on_roll=1.00000
gyro_precession_on_roll=1.00000
gyro_precession_on_yaw=1.00000


[brakes]
toe_brakes_scale=0.67100
parking_brake=1
auto_brakes=0
hydraulic_system_scalar=0.00000
differential_braking_scale=0.00000


[gear_warning_system]
gear_warning_available=0
pct_throttle_limit=0.00000
flap_limit_power=15.00000
flap_limit_idle=30.00000


[hydraulic_system]
normal_pressure=490.00000
electric_pumps=4         //no electric pumps
engine_map=1,1,1,1   //pumps on Eng1,2,3,4


[Radios]
// Radio Type=availiable, standby frequency, has glide slope
Audio.1=1
Com.1=1, 0
Com.2=1, 0
Nav.1=1, 0, 1
Nav.2=1, 0, 0
Adf.1=1
Adf.2=0
Transponder.1=0
Marker.1=0


[stall_warning]
type=1


[attitude_indicators]
attitude_indicator.0=1


[turn_indicators]
turn_indicator.0=1,0


[exits]
number_of_exits=2
exit_rate.0=0.3
exit_rate.1=0.3


[electrical]
max_generator_alternator_amps=240.0
engine_generator_map=1,1,0,0


[LIGHTS]
//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing
// longitudinal, lateral, vertical distance from datum point
light.0=3,  -3.700, -56.000,  6.050, fx_navred  // wing
light.1=3,  -3.700,  56.000,  6.050, fx_navgre  // wing
light.2=3, -39.200,  -9.500, 12.000, fx_navwhi  // fin
light.3=3, -39.200,   9.500, 12.000, fx_navwhi  // fin
light.4=3,  -3.700,  56.000,  5.100, fx_navgre  // wing
light.5=4,  14.000,   0.000, -1.200, fx_vclighth //high VC-lighting; adjust these positions as you would for the [Views] section
light.6=4,   9.000,   0.000, -1.400, fx_vclighth //flight engineer
light.7=4,   7.700,   0.000, -1.500, fx_vclighth  //cabin 1
light.8=4,  -4.000,   0.000, -1.500, fx_vclighth  //cabin 2
//light.8=4, -15.000,   0.000, -1.500, fx_vclighth  //cabin 3
light.9=4,   3.300,   0.000, -2.500, fx_vclighth //galley
//light.10=3, -39.200,  -8.800, 12.000, fx_navwhi  // fin
//light.11=3, -39.200,   8.800, 12.000, fx_navwhi  // fin
light.10=3,  -3.700, -56.000,  5.100, fx_navred  // wing
light.11=5,   2.400, -26.700,  3.920, fx_landing
light.12=5,   2.400,  26.700,  3.920, fx_landing
//light.4=3, -42.700,   0.000, -2.700, fx_navwhi  // tail cone
//light.10=4,  -8.400,   0.000, -1.000, fx_vclighth  //cabin 2
//light.11=4, -22.000,   0.000, -1.000, fx_vclighth  //cabin 4
//light.11=4,  15.500,   0.000,  2.800, fx_vclight //normal panel/VC-lighting; adjust these positions as you would for the [Views] section
//light.12=4,   8.300,   0.000, -1.500, fx_vclighth //galley


[pitot_static]
vertical_speed_time_constant=4.0              //Increasing this value will cause a more instantaneous reaction in the VSI


[GPWS]
max_warning_height=0
sink_rate_fpm=-1500
excessive_sink_rate_fpm=-2000
climbout_sink_rate_fpm=-100
flap_and_gear_sink_rate_fpm=-100


[AirWrench]
Aircraft_Length=96.90000
Vmax_sl=182.40000
Vmax_ca=190.40000
V_rc=84.60000
Climb_Rate=1087.30000
Climb_Weight=36965.00000
Max_gforce=3.70000
Emergency_hp=750.00000
VSI_Weight=29525.00000
static_margin=0.15500
nose_position_lon=33.91000
ActualIncidence=2.50000
ActualTwist=0.00000
ActualTailIncidence=1.50000
Aircraft_Type=2
ReheatCutoff=1.20000
OptimumMach=0.90000
Power_Calibration=1.00000
IdleRPM=575.00000
piston_research=0.00000
JetAltitude=0.00000
turboprop_critical_altitude=0.00000
target_roll_Vopt=523.20000
target_roll_rate=44.00000
pitch_damping=1.00000
yaw_damping=1.00000
weathervane=1.00000
elevator_scalar=1.00000
aileron_scalar=1.00000
rudder_scalar=1.00000
dihedral_scalar=1.00000
sideslip_scalar=1.00000
prop_yaw_damping_scalar=1.00000
Elevator_FF=34.90000
Aileron_FF=-38.60000
Roll_Response=30.00000
Adverse_Yaw=100.00000
Control_Response=100.00000
V_Max_Control=333.72591
V_Zero_Control=667.45182
V_Max_RdrControl=333.72591
V_Zero_RdrControl=667.45182
Spin_Stability=100.00000
Roll_Off=0.00000
glide_ratio=17.22848
CritAoA=16.00000
ClAoA_k0=1.00000
ClAoA_k1=1.00000
ClAoA_k2=0.85000
ClAoA_k3=0.80000
cruise_attitude=0.00000
Elevator_Propwash=1.00000
Rudder_Propwash=1.00000
afterburner_thrust=0.00000
prop_design_altitude=5000.00000
prop_material_type=1
protect_airfile=0
spoiler_type=0
spoiler_cd=0.00000
spoiler_cl=0.00000
spoiler_cm=0.00000
auto_flaps_enabled=0
flaps_type=1
flaps_cd_scalar=0.64419
flaps_cm_scalar=-1.11100
vfe_enabled=0
gear_cd_scalar=0.00000
gear_cm_scalar=0.00000
critical_mach_number=0.80000
max_mach_cd0=60
direct_edit_drag=0
cylinder_head_temperature=501.00000
exhaust_gas_temperature=1641.00000
fuel_pressure=26.00000
oil_pressure=60.00000
oil_temperature=241.00000
radiator_temperature=211.00000
lo_rpm_friction=1.00000
hi_rpm_friction=1.00000
exhaust_pressure_ratio=0.00000
interstage_turbine_temperature=-459.00000
RAM_Jet_Effect=1.00000
Emulate_Turbojet=0
jet_idle_scalar=1.00000
input_units=0
fs_version=5
AI_flag=0
edit_tp_torque=0
keep_jet_air_defs=0
direct_edit_mach=0
direct_edit_2dtab=0
fixed_wing_pos=0
range_est_alt=0.00000
range_est_rpm=2300.00000
range_est_mp=42.00000
range_est_fuel=1240.00000
contact_light_flags=0
AirWrenchVersion=1.01.67


[Flaps.0]
type= 1
system_type=2
span-outboard= 0.550
extending-time= 4.0
damaging-speed=0.0
blowout-speed=0.0
flaps-position.0=0.00
flaps-position.1=10.00
flaps-position.2=40.00
lift_scalar=1.00
drag_scalar=1.00
pitch_scalar=1.00

25005-S42-NC.zip

Имя файла Дата Размер
Sikorsky S-42 NC-822M/Aircraft.cfg 17.03.2009 19:55 16 KB
Sikorsky S-42 NC-822M/model/ 14.03.2009 13:55
Sikorsky S-42 NC-822M/model/Model.cfg 11.01.2009 13:26 40 B
Sikorsky S-42 NC-822M/model/Sikorsky S-42 NC-822M.mdl 14.03.2009 12:57 5 MB
Sikorsky S-42 NC-822M/panel/ 14.03.2009 13:55
Sikorsky S-42 NC-822M/panel/MainPanel2D.bmp 08.03.2009 18:54 769 KB
Sikorsky S-42 NC-822M/panel/panel.cfg 14.03.2009 13:21 11 KB
Sikorsky S-42 NC-822M/panel/S42.CAB 13.03.2009 22:51 4 MB
Sikorsky S-42 NC-822M/S-42Panel.jpg 11.03.2009 22:26 89 KB
Sikorsky S-42 NC-822M/S-42ReadMe.txt 17.03.2009 19:53 13 KB
Sikorsky S-42 NC-822M/s42-route-map-rio2.jpg 12.03.2009 22:03 122 KB
Sikorsky S-42 NC-822M/S42NC822M.jpg 11.03.2009 22:24 47 KB
Sikorsky S-42 NC-822M/Sikorsky S-42 NC-822M.air 22.02.2009 15:11 11 KB
Sikorsky S-42 NC-822M/sikorsky_s42_check.htm 11.03.2009 22:47 80 KB
Sikorsky S-42 NC-822M/sikorsky_s42_ref.htm 11.03.2009 22:48 26 KB
Sikorsky S-42 NC-822M/sound/ 14.03.2009 13:55
Sikorsky S-42 NC-822M/sound/Sound.cfg 11.03.2009 21:57 144 B
Sikorsky S-42 NC-822M/texture/ 14.03.2009 13:55
Sikorsky S-42 NC-822M/texture/CabinEntranceInteriorTextures.bmp 07.12.2008 23:27 257 KB
Sikorsky S-42 NC-822M/texture/CabinGalleyInteriorTextures.bmp 03.03.2009 20:23 257 KB
Sikorsky S-42 NC-822M/texture/CabinPassInteriorTextures.bmp 14.03.2009 13:03 257 KB
Sikorsky S-42 NC-822M/texture/CabinStewardInteriorTextures.bmp 05.03.2009 00:00 257 KB
Sikorsky S-42 NC-822M/texture/CabinTexturesSeats.bmp 08.03.2009 18:55 1 MB
Sikorsky S-42 NC-822M/texture/CockpitCeilingParts.bmp 24.02.2009 15:20 257 KB
Sikorsky S-42 NC-822M/texture/CockpitInterior.bmp 14.03.2009 12:43 1 MB
Sikorsky S-42 NC-822M/texture/Copilot.bmp 02.01.2009 20:38 257 KB
Sikorsky S-42 NC-822M/texture/FlightDeckEngineControls.bmp 23.11.2008 16:35 65 KB
Sikorsky S-42 NC-822M/texture/HorizontalTail.bmp 10.03.2009 22:44 257 KB
Sikorsky S-42 NC-822M/texture/HullMidAft.bmp 24.02.2009 15:18 1 MB
Sikorsky S-42 NC-822M/texture/HullSidesFore.bmp 24.02.2009 15:17 1 MB
Sikorsky S-42 NC-822M/texture/HullTopBottom.bmp 01.01.2009 21:21 257 KB
Sikorsky S-42 NC-822M/texture/InstPanelMainBoards.bmp 08.03.2009 00:22 257 KB
Sikorsky S-42 NC-822M/texture/InstPanels.bmp 08.03.2009 18:32 1 MB
Sikorsky S-42 NC-822M/texture/Mirror128_R.bmp 04.10.2008 01:34 16 KB
Sikorsky S-42 NC-822M/texture/NacelleCowling.bmp 10.03.2009 22:51 257 KB
Sikorsky S-42 NC-822M/texture/Pilot.bmp 02.01.2009 20:39 257 KB
Sikorsky S-42 NC-822M/texture/PilotFaces.bmp 03.03.2009 19:36 257 KB
Sikorsky S-42 NC-822M/texture/PilotHeads.bmp 03.03.2009 19:27 257 KB
Sikorsky S-42 NC-822M/texture/PropBlade_R.bmp 23.08.2008 13:23 65 KB
Sikorsky S-42 NC-822M/texture/PropDisk.bmp 11.09.2004 21:40 64 KB
Sikorsky S-42 NC-822M/texture/PWHornet1620-256.bmp 13.08.2008 01:18 65 KB
Sikorsky S-42 NC-822M/texture/Stainless_R.bmp 31.08.2008 18:36 65 KB
Sikorsky S-42 NC-822M/texture/VerticalTail.bmp 10.03.2009 14:53 257 KB
Sikorsky S-42 NC-822M/texture/Wing1024.bmp 11.03.2009 23:36 1 MB
Sikorsky S-42 NC-822M/texture/WingFloatStrut.bmp 01.09.2008 23:16 257 KB
Sikorsky S-42 NC-822M/ 14.03.2009 13:55
avsim_su.diz 10.11.2009 13:42 406 B
Итого: 20 MB
S-42 Clipper - transport flying boat, designed by designer Igor Sikorsky. Terms of Reference of the company at the Pan American transatlantic flying boat long range, received August 15, 1931, provided for the ability of an aircraft carrying a crew of four and 12 passengers to a distance of 4023 kilometers (2500 miles) with a cruising speed of 233 kilometers per hour (145 miles / hour) . November 30, 1932 the airline signed a contract with Martin to design aircraft M-130 and with the firm on a plane Sikorski S-42. S-42 had a traditional building flying boat and was equipped with four engines, Pratt & Whitney Hornet S5D1G engine with 700 hp. The first aircraft was delivered in August 1934 at the base of the company Pan American, and the first shuttle flight took place on 16 August.
→ Size: 9 MB
→ Date: 16 years ago (10.11.2009 12:55)
→ Author: George Diemer
→ Approved by moderator: omega
→ License: Freeware - Free version, Unlimited Distribution
→ Downloaded: 2209 time(s)