//C133B CARGOMASTER 

[fltsim.0]
title=C-133B Cargomaster MATS
sim=C-133B_CARGOMASTER
model=
panel=
sound=
texture=
panel_alias =
sound_alias =
kb_checklists=C-133B_check
kb_reference=
visual_damage=1
atc_id=
atc_id_color=0xffffffff
atc_airline =
atc_flight_number =
ui_manufacturer=Douglas
ui_type=C133B Cargomaster
ui_variation=USAF Military Air Transport Service ( MATS )
description=The Douglas C-133B Cargomaster Long Range Strategic Airlifter made its first flight on April 23, 1956.  It was formed along the same lines as the well-known C-130 Hercules, but was a much larger aircraft.  It was able to transport nearly every contemporary vehicle in service at the time with the United States Army due to its enormous size and large loading doors.  The last three aircraft built had special clamshell doors which extended the cargo area by 3 feet, allowing a completely assembled Titan missile to be transported.  The fleet of 50 aircraft provided excellent service up until 1971, when they were withdrawn due to fatigue problems.  A number of aircraft were later released to the civilian market.
atc_heavy=0

[General]
atc_type= 
atc_name=douglas
performance = * Weight: 117419 lbs    Max 282000 lbs * Power: 7500 hp * Max speed @ SL: 308 mph * Max speed: 355 mph @ 20000 ft * Climb rate: 3475 ft/min @ 197 mph Flight Model By: Tim Piglet Conrad Piglet's Peculiar Planes 8/6/03 12:28 AM Flight Model Workbook V2.82.98
editable=1 
atc_model=

[exits]
number_of_exits = 2
exit_rate.0 = 0.4                               ;Percent per second
exit_rate.1 = 0.4                               ;Percent per second

[weight_and_balance]

// ACM V2.3
max_gross_weight = 286000.000
empty_weight = 120263.000
reference_datum_position = 0.000, 0.000, 0.000
empty_weight_CG_position = -0.460, 0.000, 0.000
empty_weight_pitch_MOI = 3690324.000
empty_weight_roll_MOI = 1883757.000
empty_weight_yaw_MOI = 4221328.000
empty_weight_coupled_MOI = 0.000
max_number_of_stations = 6

station_load.0 =200.000000, 60.770000, -2.000000, 2.150000, Station 1
station_load.1 =200.000000, 60.770000, 2.000000, 2.150000, Station 2
station_load.2 =200.000000, 56.540000, -2.000000, 2.270000, Station 3
station_load.3 =200.000000, 56.540000, 2.000000, 2.270000, Station 4
station_load.4 =200.000000, 48.000000, 2.000000, 0.000000, Station 5
station_load.5 =100.000000, 0.000000, 0.000000, 0.000000, Station 6
CG_forward_limit= 0.000
CG_aft_limit= 1.000


[lights]

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

light.0 = 1, -67.342, 0, 38.142, fx_beacon
light.1 = 1, 20.359, 0, -8.755, fx_beacon
light.2 = 3, -3.016, -85.663, 12.574, fx_navred
light.3 = 3, -3.016, 85.663, 12.574, fx_navgre
light.4 = 3, -86.332, -0.293, 10.218, fx_navwhi
light.5 = 3, -24.391, 0, 8.039, fx_navwhi
light.6 = 3, -24.385, 0, -8.773, fx_navwhi
light.7 = 4, 57, 0, 3, fx_vclight

[GeneralEngineData]

//0=Piston, 1=Jet, 2=None, 3=Helo-Turbine, 4=Rocket, 5=Turboprop
engine_type = 5
fuel_flow_scalar = 0.7305
engine.0 = 14.750, -40.200, 0.000
engine.1 = 15.750, -20.500, 0.000
engine.2 = 15.750, 20.500, 0.000
engine.3 = 14.750, 40.200, 0.000
min_throttle_limit=-0.250000

[effects]
wake = fx_wake
water = fx_spray
dirt = fx_tchdrt
concrete = fx_sparks

[smokesystem]
    smoke.0 = -5.19, -30, 41.39, fx_smoke_rx1
    smoke.1 = -5.06, -32, 22.27, fx_smoke_rx1
    smoke.2 = -5.06, -32, -22.27, fx_smoke_rx1
    smoke.3 = -5.19, -30, -41.39, fx_smoke_rx1


[fuel]

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

fuel_type = 2
number_of_tank_selectors = 1

LeftMain = 0.000, -13.000, 0.000, 5400.000, 0.000
LeftAux = 0.000, -30.000, 0.000, 1839.000, 0.000
RightMain = 0.000, 13.000, 0.000, 5400.000, 0.000
RightAux = 0.000, 30.000, 0.000, 1839.000, 0.000
electric_pump=0


[contact_points]
static_pitch = -1.125
static_cg_height = 12.140
max_number_of_points = 9

point.0 = 1.000, 57.000, 0.000, -11.000, 2500.000, 0.000, 1.750, 40.000, 0.050, 3.000, 0.850, 5.000, 5.000, 0.000, 0.000, 0.000
point.1 = 1.000, -1.500, -7.500, -12.200, 2500.000, 1.000, 2.500, 0.000, 0.400, 2.500, 0.800, 5.000, 5.000, 2.000, 0.000, 0.000
point.2 = 1.000, -1.500, -10.000, -12.200, 2500.000, 1.000, 2.500, 0.000, 0.400, 2.500, 0.800, 5.000, 5.000, 2.000, 0.000, 0.000
point.3 = 1.000, -1.500, 7.500, -12.200, 2500.000, 2.000, 2.500, 0.000, 0.400, 2.500, 0.800, 5.000, 5.000, 3.000, 0.000, 0.000
point.4 = 1.000, -1.500, 10.000, -12.200, 2500.000, 2.000, 2.500, 0.000, 0.400, 2.500, 0.800, 5.000, 5.000, 3.000, 0.000, 0.000
point.5 = 2.000, -3.233, -85.262, 12.615, 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.6 = 2.000, -3.076, 85.261, 12.580, 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.7 = 2.000, -31.489, 0.000, -9.276, 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.8 = 2.000, 63.844, 0.000, -4.212, 1574.803, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 4.000, 0.000, 0.000
gear_system_type=0


[keyboard_response]
elevator = 350.000000, 500.000000
aileron = 450.000000, 1000.000000
rudder = 200.000000, 1000.000000


[forcefeedback]
gear_bump_nose_magnitude = 1000
gear_bump_nose_direction = 18000
gear_bump_nose_duration = 250000
gear_bump_left_magnitude = 2000
gear_bump_left_direction = 35500
gear_bump_left_duration = 250000
gear_bump_right_magnitude = 2000
gear_bump_right_direction = 500
gear_bump_right_duration = 250000
ground_bumps_magnitude1 = 1250
ground_bumps_angle1 = 8900
ground_bumps_intercept1 = 5
ground_bumps_slope1 = 0.48
ground_bumps_magnitude2 = 450
ground_bumps_angle2 = 9100
ground_bumps_intercept2 = 0.075
ground_bumps_slope2 = 1
crash_magnitude1 = 2000
crash_direction1 = 1000
crash_magnitude2 = 2000
crash_direction2 = 9000
crash_period2 = 7500
crash_duration2 = 2500000
stick_shaker_magnitude = 2000
stick_shaker_direction = 0
stick_shaker_period = 111111

[airplane_geometry]
wing_area = 2673.000
wing_span = 179.000
wing_root_chord = 23.690
wing_dihedral = 4.000
wing_incidence = 0.000
wing_twist = 0.000
oswald_efficiency_factor = 0.850
wing_winglets_flag = 1
wing_sweep = 4.000
wing_pos_apex_lon = 6.680
wing_pos_apex_vert = 6.650
htail_area = 450.000
htail_span = 58.040
htail_pos_lon = -58.520
htail_pos_vert = 0.000
htail_incidence = 1.750
htail_sweep = 17.500
vtail_area = 410.000
vtail_span = 27.130
vtail_sweep = 28.000
vtail_pos_lon = -52.220
vtail_pos_vert = 10.720
elevator_area = 365.000
aileron_area = 130.000
rudder_area = 205.000
elevator_up_limit = 27.502
elevator_down_limit = 20.626
aileron_up_limit = 19.481
aileron_down_limit = 14.897
rudder_limit = 23.491
elevator_trim_limit = 15.000
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 = 24
generator_alternator_voltage = 28
max_generator_alternator_amps = 60
electric_always_available = 0
flap_motor = 0, 5, 17
gear_motor = 0, 5, 17
autopilot = 0, 5, 17
avionics_bus = 0, 10, 17
avionics = 1, 5, 17
pitot_heat = 0, 2, 17
additional_system = 0, 20, 17
marker_beacon = 1, 2, 17
gear_warning = 0, 2, 17
fuel_pump = 0, 5, 17
starter1 = 0, 20, 17
light_nav = 0, 5, 17
light_beacon = 0, 5, 17
light_landing = 0, 5, 17
light_taxi = 0, 5, 17
light_strobe = 0, 5, 17
light_panel = 0, 5, 17

[direction_indicators]
direction_indicator.0=3,0 


[Reference Speeds]	//aircraft weight 183,500 lbs.
flaps_up_stall_speed= 107.000 
full_flaps_stall_speed= 87.000 
cruise_speed= 280.000 
never_exceed_speed=325.00000
max_indicated_speed=325.000000
max_mach=0.65

[TurbineEngineData]
fuel_flow_gain=0.006 
inlet_area= 5.55
rated_N2_rpm= 29920.000 
static_thrust= 3000.000 
afterburner_available= 0

[turboprop_engine]
maximum_torque= 39389

[propeller]
rotation= 1, 1, -1, -1 
propeller_type= 0 
propeller_diameter= 19.400 
propeller_blades= 3 
propeller_moi= 192.000 
beta_max= 45.000 
beta_min= 12.000 
min_gov_rpm= 25520.000 
prop_tc= 0.004 
gear_reduction_ratio= 29.92
fixed_pitch_beta= 0.000 
low_speed_theory_limit= 80.000 
prop_sync_available= 1 
prop_deice_available= 1 
prop_feathering_available= 1 
prop_auto_feathering_available= 1 
min_rpm_for_feather= 700.000 
beta_feather= 80.000 
power_absorbed_cf= 0.900 
defeathering_accumulators_available= 0 
prop_reverse_available= 1.000 
minimum_on_ground_beta= 0.000 
minimum_reverse_beta= -14.000 

[Views]
eyepoint=60.475, -2.127, 4.0 

[autopilot]
autopilot_available=1 
flight_director_available=1 
default_vertical_speed=500 
autothrottle_available=1 
autothrottle_arming_required=0
autothrottle_max_rpm = 90
autothrottle_takeoff_ga=1
pitch_takeoff_ga=8 ; 
max_pitch=10.000000
max_pitch_acceleration=1.000000
max_pitch_velocity_lo_alt=2.000000
max_pitch_velocity_hi_alt=1.500000
max_pitch_velocity_lo_alt_breakpoint=20000.000000
max_pitch_velocity_hi_alt_breakpoint=28000.000000
max_bank=25.000000
max_bank_acceleration=1.800000
max_bank_velocity=3.000000
max_throttle_rate=0.100000
nav_proportional_control=9.000000
nav_integrator_control=0.250000
nav_derivative_control=0.000000
nav_integrator_boundary=2.500000
nav_derivative_boundary=0.000000
gs_proportional_control=9.520000
gs_integrator_control=0.260000
gs_derivative_control=0.000000
gs_integrator_boundary=0.700000
gs_derivative_boundary=0.000000
yaw_damper_gain=0.000000

[brakes]
toe_brakes_scale=0.856
parking_brake=1
[gear_warning_system]
gear_warning_available=1
pct_throttle_limit=0.099976
flap_limit_power=30.022988
flap_limit_idle=15.011494
[hydraulic_system]
electric_pumps=0
engine_map=1,1,1,1
normal_pressure=3000.000000
[stall_warning]
type=1
[attitude_indicators]
attitude_indicator.0=1
[turn_indicators]
turn_indicator.0=1,0

[Flaps.0]
type= 1
span-outboard= 0.5
extending-time= 5.000
system_type= 1
damaging-speed= 175
blowout-speed= 225
lift_scalar= 1.000
drag_scalar= 1.000
pitch_scalar= 1.000
flaps-position.0= 0.000, 0.000
flaps-position.1= 15.000, 0.000
flaps-position.2= 25.000, 0.000
flaps-position.3= 35.000, 0.000
flaps-position.4= 45.000, 0.000

[Radios]
Audio.1=1
Com.1=1,1
Com.2=1,1
Nav.1=1,1,1
Nav.2=1,1,1
Adf.1=1,0
Transponder.1=1
Marker.1=1
