[fltsim.0]
title=B-24D Liberator
sim=B24D_Liberator
model=
panel=
sound=
texture=

ui_manufacturer=Consolidated
ui_type=B-24D Liberator
ui_variation=Olive Drab (Army)
atc_heavy=0
atc_id=42-72843
atc_airline=Army
atc_flight_number=843

description=The Consolidated B-24 was employed in operations in every combat theater during the war. Because of its great range, it was particularly suited for such missions as the famous raid from North Africa against the oil industry at Ploesti, Rumania on August 1, 1943. This feature also made the airplane suitable for long over-water missions in the Pacific Theater. More than 18,000 Liberators were produced.

[WEIGHT_AND_BALANCE]
empty_weight= 37000.000

reference_datum_position= 0.000, 0.000, 0.000
empty_weight_CG_position= 6.500, 0.000, 0.000

max_number_of_stations=50

station_load.0= 170.000, 8.000, -4.000, 2.000
station_load.0=170,  8.0,  4.0, 2.0		//Co-Pilot        Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)

;Moments of Inertia
empty_weight_pitch_MOI= 187288.650
empty_weight_roll_MOI= 217421.290
empty_weight_yaw_MOI= 343138.880
empty_weight_coupled_MOI= 0.000
max_gross_weight= 51234.060
CG_forward_limit= 0.000
CG_aft_limit= 1.000



[flight_tuning]
cruise_lift_scalar=1.500
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

[piston_engine]
power_scalar=1.541
cylinder_displacement= 130.700
compression_ratio= 6.700
number_of_cylinders= 14
max_rated_rpm= 2700.000
max_rated_hp= 1200.000
fuel_metering_type= 0
cooling_type= 0
normalized_starter_torque= 0.035
turbocharged= 1
max_design_mp= 46.000
min_design_mp= 1.000
critical_altitude= 17000.000
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=1.511
propeller_type= 0
propeller_diameter= 10.833
propeller_blades= 3
propeller_moi= 33.370
beta_max= 53.500
beta_min= 18.500
min_gov_rpm= 1800.000
prop_tc= 0.010
gear_reduction_ratio= 1.778
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
minimum_on_ground_beta= 0.000
minimum_reverse_beta= 0.000

[electrical]
max_battery_voltage=24.0
generator_alternator_voltage=28.0
max_generator_alternator_amps=60.0

[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	         (0=Undamped, 1=Critically Damped)
//11 Extension Time	         (seconds)
//12 Retraction Time	         (seconds)
//13 Sound Type

point.0= 1.000, 15.500, 0.000, -12.300, 1400.000, 0.000, 1.500, 42.700, 1.060, 2.500, 0.700, 6.000, 7.000, 0.000, 0.000, 0.000
point.1= 1.000, -1.500, -13.170, -12.000, 2000.000, 1.000, 2.500, 0.000, 1.060, 2.500, 0.860, 7.500, 8.500, 2.000, 0.000, 0.000
point.2= 1.000, -1.500, 13.170, -12.000, 2000.000, 2.000, 2.500, 0.000, 1.060, 2.500, 0.860, 7.000, 8.000, 3.000, 0.000, 0.000
point.3= 2.000, 0.000, -55.830, 1.000, 800.000, 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, 0.000, 55.830, 1.000, 800.000, 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, -39.580, 0.000, -2.830, 800.000, 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, 17.160, 0.000, -4.830, 800.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 4.000, 0.000, 0.000

static_cg_height= 10.780
static_pitch= 2.410

[General]
performance=SPECIFICATIONS \nSpan: 110 ft. 0 in. \nLength: 66 ft. 4 in. \nHeight: 17 ft. 11 in. \nWeight: 56,000 lbs. loaded \nArmament: Ten .50-cal. machine guns and 8,000 lbs. of bombs \nEngines: Four Pratt & Whitney R-1830s of 1,200 hp. ea. \nCost: $336,000 \nSerial Number: 42-72843 \n\nPERFORMANCE \nMaximum speed: 303 mph. \nCruising speed: 175 mph. \nRange: 2,850 mph. \nService Ceiling: 28,000 ft. \n\nBy: Adam Warren
atc_type=EXPERIMENTAL
atc_model=B24D

[forcefeedback]
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

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

NOTES: Original "White Smoke" Settings below:
To activate the original white smoke, remove the slash (/)
from the begining of the 3 lines of text below.  If you activate
the white smoke, you must de-activate the black smoke by
adding a slash(/) at the begining of each line of text below.

/[SMOKESYSTEM]
/smoke.0=2.70,-1.4,-9.3, fx_smoke_w                                      
/smoke.1=2.70,-1.4,9.3, fx_smoke_w
/smoke.2=2.70,-1.4,-25.3, fx_smoke_w                                      
/smoke.3=2.70,-1.4,25.3, fx_smoke_w



NOTES: "Black Exhaust Smoke" Settings below:
To activate the black smoke settings, remove the slash (/)
from the begining of the 3 lines of text below.  If you activate
the black smoke, you must de-activate the white smoke by
adding a slash(/) at the begining of each line of text below.

[SMOKESYSTEM]
smoke.0=2.70,-1.4,-9.3, fx_smoke_rx
smoke.1=2.70,-1.4,9.3, fx_smoke_rx
smoke.2=2.70,-1.4,-25.3, fx_smoke_rx
smoke.3=2.70,-1.4,25.3, fx_smoke_rx

[fuel]
Center1= 2.000, 0.000, -1.170, 1562.670, 0.000
LeftMain= -2.330, -22.400, 0.230, 390.670, 0.000
RightMain= -2.330, 22.400, 0.230, 390.670, 0.000
fuel_type=1.000000
number_of_tank_selectors=1

[airplane_geometry]
wing_area= 1048.000
wing_span= 110.000
wing_root_chord= 9.417
wing_dihedral= 3.999
wing_incidence= 1.000
wing_twist= 0.000
oswald_efficiency_factor= 0.750
wing_winglets_flag= 0
wing_sweep= 0.000
wing_pos_apex_lon= 0.000
wing_pos_apex_vert= 0.000
htail_area= 331.000
htail_span= 43.000
htail_pos_lon= -38.750
htail_pos_vert= 0.000
htail_incidence= -2.000
htail_sweep= 0.000
vtail_area= 220.000
vtail_span= 16.912
vtail_sweep= 0.000
vtail_pos_lon= -38.750
vtail_pos_vert= 7.167
elevator_area= 94.410
aileron_area= 80.250
rudder_area= 39.490
elevator_up_limit= 28.000
elevator_down_limit= 22.999
aileron_up_limit= 26.001
aileron_down_limit= 18.999
rudder_limit= 28.000
elevator_trim_limit= 19.996
spoiler_limit= 0.000
spoilerons_available= 0
aileron_to_spoileron_gain= 0.000
min_ailerons_for_spoilerons= 0.000
min_flaps_for_spoilerons= 0.000

[GeneralEngineData]
engine_type= 0
Engine.0= 9.333, -25.417, 0.250
Engine.1= 10.333, -11.167, 0.000
Engine.2= 10.333, 11.167, 0.000
Engine.3= 9.333, 25.417, 0.250
fuel_flow_scalar= 1.000

[Reference Speeds]
flaps_up_stall_speed= 110.000
full_flaps_stall_speed= 88.000
cruise_speed= 242.458

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

[Views]
eyepoint=-4.562418,0.000000,3.216761

[autopilot]
autopilot_available=1
flight_director_available=0
default_vertical_speed=700.000000
autothrottle_available=0
pitch_takeoff_ga=8.000000

[direction_indicators]
direction_indicator.0=1,0

[Flaps.0]
type= 1
span-outboard= 0.500
extending-time= 5.000
system_type= 0
damaging-speed= 0.000
blowout-speed= 0.000
lift_scalar= 1.500
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= 30.000, 0.000
flaps-position.3= 45.000, 0.000