[fltsim.0]
title=Ayres Turbo Thrush MRCU
sim=Thrush
model=5-blades
panel=
sound=
texture=MRCU
panel_alias =
sound_alias = C208\sound
kb_checklists=
kb_reference=
atc_id=VP-CKF
atc_id_color=0xff000000
ui_manufacturer=Ayres
ui_type=Turbo Thrush
ui_variation=MRCU 'Mosquito Research and Control Unit'
description=Turbine powered agricultural aircraft.\n\nEngine: Pratt & Whitney PT6A-34AG (750 shp)\nHopper capacity: 510 Gallon (1938 lit)
atc_parking_types=RAMP
atc_heavy=0
atc_airline=
atc_flight_number=
prop_anim_ratio=0.8
[General]
atc_type=ROCKWELL
atc_model=
performance=Never exceed speed: 159 MPh\nStall speed (empty, flaps down): 57 MPh\nWorking Speed: 90 - 150 MPh\n
Category=airplane
[WEIGHT_AND_BALANCE]
max_gross_weight = 9700.000
empty_weight = 4300.000
reference_datum_position = 12.424, 0.000, 0.000
empty_weight_CG_position = -11.000, 0.000, -2.000
max_number_of_stations = 3
station_load.0 =2200.000000, -11.000000, 0.000000, 0.000000, Hopper
station_load.1 =170.000000, -17.000000, 0.000000, 0.000000, Pilot
station_load.2=0.000000, 0.000000, 0.000000, 0.000000, Crew
;Moments of Inertia
empty_weight_pitch_MOI = 6939.000
empty_weight_roll_MOI = 3000.000
empty_weight_yaw_MOI = 8923.000
empty_weight_coupled_MOI = 0.000
CG_forward_limit= 0.000
CG_aft_limit= 1.000
[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
[GeneralEngineData]
engine_type = 5
Engine.0 = -2.700, 0.000, 0.000
fuel_flow_scalar = 1.120
min_throttle_limit = -0.25 //Minimum percent throttle. Generally negative for turbine reverser
master_ignition_switch=1
[propeller]
thrust_scalar =1.000
propeller_type = 0
propeller_diameter = 8.800
propeller_blades = 3
propeller_moi = 19.000
beta_max = 45.000
beta_min = 15.600
min_gov_rpm = 25520.000
prop_tc = 0.004
gear_reduction_ratio = 17.400
fixed_pitch_beta = 0.000
low_speed_theory_limit = 80.000
prop_sync_available = 0
prop_deice_available = 0
prop_feathering_available= 1
prop_auto_feathering_available= 1
min_rpm_for_feather = 700.000
beta_feather = 88.000
power_absorbed_cf = 0.900
defeathering_accumulators_available= 0
prop_reverse_available = 1.000
minimum_on_ground_beta = 1.000
minimum_reverse_beta = -14.000
[TurbineEngineData]
fuel_flow_gain = 0.011
inlet_area = 1.000
rated_N2_rpm = 33000.000
static_thrust = 158.000
afterburner_available= 0
[turboprop_engine]
power_scalar =1.000
maximum_torque = 1865.000
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
[pitot_static]
vertical_speed_time_constant = 1.0 //Increasing this value will cause a more instantaneous reaction in the VSI
pitot_heat=1.000000
[Radios]
// Radio Type = availiable, standby frequency, has glide slope
Audio.1 = 0
Com.1 = 1, 1
Com.2 = 1, 1
Nav.1 = 0, 0, 0
Nav.2 = 0, 0, 0
Adf.1 = 0
Transponder.1 = 0
Marker.1 = 0
[LIGHTS]
//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit
light.0 = 3, -12.00, -23.8, 0.74, fx_navred
light.1 = 3, -12.00, 23.8, 0.74, fx_navgre
light.2 = 3, -27.80, 0.00, 6.7, fx_navwhi
light.3 = 2, -12.00, -23.8, 0.74, fx_strobe
light.4 = 2, -12.00, 23.8, 0.74, fx_strobe
light.5 = 4, -16.50, 0, 3.00, fx_vclight
[keyboard_response]
//Breakpoint speeds (knots) on the keyboard increments of control surfaces.
//Speed at which the incremenet is reduced to 1/2 and 1/8 respectively.
elevator = 100, 180
aileron = 200, 1000
rudder = 200, 1000
[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=0,0
[attitude_indicators]
//Type: 0=None, 1=Vacuum Gyro, 2=Electric Gyro
attitude_indicator.0 = 0
[turn_indicators]
//Type: 0=None, 1=Electric Gyro, 2= Vacuum Gyro
turn_indicator.0=0,0
[electrical]
flap_motor = 0, 5 , 17.0
avionics_bus = 0, 5 , 17.0
avionics = 1, 5 , 17.0
pitot_heat = 0, 2 , 17.0
additional_system = 0, 2 , 17.0
fuel_pump = 0, 5 , 17.0
starter1 = 0, 20, 17.0
light_nav = 0, 5 , 17.0
light_strobe = 0, 5 , 17.0
light_panel = 0, 5 , 17.0
//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
[contact_points]
static_pitch= 13.500
static_cg_height= 4.750
max_number_of_points=10
gear_system_type=0 //Fixed
point.0= 1.000, -28.200, 0.000, -1.355, 9000.000, 0.000, 0.500, 90.000, 0.200, 1.500, 0.900, 0.000, 0.000, 0.000, 0.000, 0.000
point.1= 1.000, -9.840, -4.675, -5.750, 3000.000, 1.000, 0.750, 0.000, 0.500, 2.500, 0.850, 0.000, 0.000, 0.000, 0.000, 0.000
point.2= 1.000, -9.840, 4.675, -5.750, 3000.000, 2.000, 0.750, 0.000, 0.500, 2.500, 0.850, 0.000, 0.000, 0.000, 0.000, 0.000
point.3= 2.000, 0.000, 0.000, 0.000, 10000.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 4.000, 0.000, 0.000
point.4= 2.000, -11.500, 0.000, -1.800, 10000.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 4.000, 0.000, 0.000
point.5= 2.000, -30.000, 0.000, 1.300, 10000.000, 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, -18.000, -22.000, -0.560, 10000.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 5.000, 0.000, 0.000
point.7= 2.000, -18.000, 22.000, -0.560, 10000.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 6.000, 0.000, 0.000
point.8= 2.000, -17.700, 0.000, 5.200, 10000.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 4.000, 0.000, 0.000
[gear_warning_system]
gear_warning_available = 0 //Normal
pct_throttle_limit = 0.1 //Percent throttle that activates warning
flap_limit_idle = 0.0 //Flap angle that activates warning at idle
flap_limit_power = 16.0 //Flap angle that activates warning at above idle
[brakes]
parking_brake = 1 //Parking brake available
toe_brakes_scale = 0.75 //Brake scalar
differential_braking_scale=1
[hydraulic_system]
normal_pressure = 3000.0 //PSI
electric_pumps = 0 //no electric pumps
engine_map =1,0,0,0
[Views]
eyepoint= -17.3, 0, 4.63 //(feet) longitudinal, lateral, vertical distance from reference datum
[fuel]
LeftMain = -12.000, -4.800, -0.850, 114.000, 3.600
RightMain = -12.000, 4.800, -0.850, 114.000, 3.600
fuel_type = 2 //Fuel type: 1 = Avgas, 2 = JetA
number_of_tank_selectors = 1
electric_pump=1
[EFFECTS]
wake=fx_wake
water=fx_spray
dirt=fx_tchdrt
concrete=fx_sparks
touchdown=fx_tchdwn_s, 1
[smokesystem]
smoke.0=0.00, -20.00, -19.00, fx_thrush_spray_tip_minus
smoke.1=0.00, -20.00, -16.00, fx_thrush_spray
smoke.2=0.00, -20.00, -13.20, fx_thrush_spray
smoke.3=0.00, -20.00, -10.40, fx_thrush_spray
smoke.4=0.00, -20.00, -7.60, fx_thrush_spray
smoke.5=0.00, -20.00, -4.80, fx_thrush_spray
smoke.6=0.00, -20.00, -2.00, fx_thrush_spray
smoke.7=0.00, -20.00, 2.00, fx_thrush_spray
smoke.8=0.00, -20.00, 4.80, fx_thrush_spray
smoke.9=0.00, -20.00, 7.60, fx_thrush_spray
smoke.10=0.00, -20.00, 10.40, fx_thrush_spray
smoke.11=0.00, -20.00, 13.20, fx_thrush_spray
smoke.12=0.00, -20.00, 16.00, fx_thrush_spray
smoke.13=0.00, -20.00, 19.00, fx_thrush_spray_tip_plus
[exits]
number_of_exits = 1
exit_rate.0 = 0.4 ;Percent per second
[airplane_geometry]
wing_area = 326.600
wing_span = 44.500
wing_root_chord = 7.340
wing_dihedral = 2.000
wing_incidence = 1.500
wing_twist = 0.000
oswald_efficiency_factor= 0.700
wing_winglets_flag = 0
wing_sweep = 0.000
wing_pos_apex_lon = -8.000
wing_pos_apex_vert = -0.850
htail_area = 22.660
htail_span = 16.010
htail_pos_lon = -40.000
htail_pos_vert = 2.300
htail_incidence = 0.000
htail_sweep = 0.000
vtail_area = 21.800
vtail_span = 4.300
vtail_sweep = 0.000
vtail_pos_lon = -26.200
vtail_pos_vert = 4.600
elevator_area = 23.700
aileron_area = 100.000
rudder_area = 14.130
elevator_up_limit = 28.000
elevator_down_limit = 21.000
aileron_up_limit = 25.000
aileron_down_limit = 15.000
rudder_limit = 35.000
elevator_trim_limit = 19.500
spoiler_limit = 0.000
spoilerons_available = 0
aileron_to_spoileron_gain = 1.000
min_ailerons_for_spoilerons = 0.000
min_flaps_for_spoilerons = 0.000
auto_spoiler_available=0
positive_g_limit_flaps_up=4.000000
positive_g_limit_flaps_down=2.000000
negative_g_limit_flaps_up=-1.500000
negative_g_limit_flaps_down=-1.500000
[Reference Speeds]
flaps_up_stall_speed = 61.000
full_flaps_stall_speed = 59.000
cruise_speed = 130.000
max_mach = 0.60
max_indicated_speed= 138.000
[autopilot]
autopilot_available= 0
flight_director_available= 0
default_vertical_speed= 1000.0
autothrottle_available= 0
max_pitch=10.0
max_pitch_acceleration=1.0
max_pitch_velocity_lo_alt=2.0
max_pitch_velocity_hi_alt=1.5
max_pitch_velocity_lo_alt_breakpoint=20000.0
max_pitch_velocity_hi_alt_breakpoint=28000.0
max_bank=25.0
max_bank_acceleration=1.8
max_bank_velocity=3.00
max_throttle_rate=0.10
nav_proportional_control=9.00
nav_integrator_control=0.25
nav_derivative_control=0.00
nav_integrator_boundary=2.50
nav_derivative_boundary=0.00
gs_proportional_control=9.52
gs_integrator_control=0.26
gs_derivative_control=0.00
gs_integrator_boundary=0.70
gs_derivative_boundary=0.00
yaw_damper_gain = 1.0
pitch_takeoff_ga= 8.000
[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
[stall_warning]
type=1
stick_shaker=0
[Flaps.0]
type= 1
span-outboard= 0.500
extending-time= 5.700
system_type= 0
damaging-speed= 200.000
blowout-speed= 200.000
lift_scalar= 1.000
drag_scalar= 1.900
pitch_scalar= 1.000
flaps-position.0= 0.000, 0.000
flaps-position.1= 10.000, 0.000
flaps-position.2= 25.000, 0.000
[vacuum_system]
max_pressure=5.150000
vacuum_type=2
electric_backup_pressure=0.000000
engine_map=0,0,0,0
[pneumatic_system]
max_pressure=18.000000
bleed_air_scalar=0.150000
[deice_system]
structural_deice_type=2
