// Title:	An-24RV dynamics
// Author:	Curl-Aless
// Version:	v41_1
// Date:	June 2005

[fltsim.0]
title=An-24RV
sim=Antonov An-24RV
model=
panel=
sound=
texture=utair
kb_reference=An-24RV_flight_instructions
ui_manufacturer=Antonov
ui_type=Antonov An-24RV
ui_variation=Aeroflot
description=FS2002 PRO Antonov An-24BFlight Dynamics by Peter Yashin2002 (c)mail to: [email protected]       
visual_damage=1

[fltsim.1]
title=An-24RV Aeroflot noVC
sim=Antonov An-24RV
model=noVC
panel=noVC
sound=
texture=utair
kb_reference=An-24RV_flight_instructions
ui_manufacturer=Antonov
ui_type=Antonov An-24RV
ui_variation=Aeroflot (no VC)
description="The legendary Russian turboprop"
visual_damage=1

// --- add custom liveries starting from here ---
// [fltsim.1]
// ...

// --- do not modify after this line ---
[General]
performance=48 Passenger\nTwin Turboprop\nRegional Commuter\n\nDevelopment version
atc_type=Antonov
atc_model=AN24

[GeneralEngineData]
engine_type=5
Engine.0=8.3, -12.956, 3.0
Engine.1=8.3, 12.956, 3.0
fuel_flow_scalar=0.944
min_throttle_limit=-0.01

[Propeller]
thrust_scalar=1.2 //1.3 //1.08
propeller_type=0
propeller_diameter=12.795
propeller_blades=4
propeller_moi=350
beta_max=49.99
beta_min=8.0
min_gov_rpm=13900.00
prop_tc=0.009
gear_reduction_ratio=12.1285
fixed_pitch_beta=15
low_speed_theory_limit=180.000
prop_sync_available=1
prop_deice_available=1
prop_feathering_available=1
prop_auto_feathering_available=1
min_rpm_for_feather=500.000
beta_feather=93.320
power_absorbed_cf=1.000
defeathering_accumulators_available=0
prop_reverse_available=1
minimum_on_ground_beta=0.0
minimum_reverse_beta=0.0 //19.0 for LSL
rotation=-1 -1

[Turboprop_engine]
power_scalar=1.0 
maximum_torque=10614.3602
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

[TurbineEngineData]
fuel_flow_scalar=1.0000
fuel_flow_gain=0.0030
inlet_area=1.000
rated_N2_rpm= 15100
static_thrust=625
afterburner_available=0

[flight_tuning]
cruise_lift_scalar=1.09 
pitch_stability=1.1
roll_stability=0.900
yaw_stability=1.000
parasite_drag_scalar=1.0
induced_drag_scalar=1.0
elevator_effectiveness=0.45 //1.0
aileron_effectiveness=0.50
rudder_effectiveness=0.60
elevator_trim_effectiveness=0.55
aileron_trim_effectiveness=1.000
rudder_trim_effectiveness=1.000

[forcefeedback]
stick_shaker_magnitude=5000		; 0 - 10000
stick_shaker_direction=0		; 0 - 35999 degrees
stick_shaker_period=111111		; in microseconds
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=9000		; 0 - 35999 degrees
gear_bump_left_duration=250000		; in microseconds
gear_bump_right_magnitude=2700		; 0 - 10000
gear_bump_right_direction=27000		; 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

[Weight_and_balance]
MTW=47398.47 //21500 kg
MLW=47398.47  //21500 kg
empty_weight=31260.94  //14180 kg 
empty_weight_cg_position=-3.1, 0.000, 0.0
reference_datum_position=0.00, 0.000, 0.000
empty_weight_roll_MOI=149345.2
empty_weight_pitch_MOI=223887.1
empty_weight_yaw_MOI=295687.8
empty_weight_coupled_MOI=1800.000
max_gross_weight=47398.47   //21500kg
CG_forward_limit=-2.7
CG_aft_limit=-4.32

max_number_of_stations=50
station_load.0=2270.66,-4.1,0.000000,0.000000
station_load.1=8270.66,-6.3,0.000000,0.000000

[electrical]
max_battery_voltage=27
generator_alternator_voltate=28.5
max_generator_alternator_amps=600.0
flap_motor=0, 5 , 17.0
gear_motor=0, 5 , 17.0
autopilot=0, 5 , 17.0
avionics_bus=0, 10, 17.0
avionics=1, 5 , 17.0
pitot_heat=0, 15, 17.0
additional_system=0, 2 , 17.0
marker_beacon=1, 2 , 17.0
gear_warning=0, 2 , 17.0
fuel_pump=0, 5 , 17.0
starter1=0, 20, 17.0
starter2=0, 20, 17.0
light_nav=0, 5 , 10.0
light_beacon=0, 5 , 10.0
light_landing=0, 5 , 17.0
light_taxi=0, 5 , 17.0
light_strobe=0, 5 , 10.0
light_panel=0, 5 , 10.0

[fuel]
LeftMain=-4.244, -17.400, 4.300, 483.41, 0.000 //1469kg 
LeftAux=-4.244, -10.000, 4.3, 304.73, 0.000 //926kg
RightMain=-4.244, 17.400, 4.3, 483.41, 0.000 //1469kg
RightAux=-4.244, 10.000, 4.3, 304.73, 0.000 //926kg
fuel_type=2.000000
number_of_tank_selectors=2
electric_pump=0

[airplane_geometry]
wing_area=802.073 //- real //1012 
wing_span=87.725 //- real //110
wing_root_chord=9.2
wing_dihedral=0.000
wing_incidence=1.3
wing_twist=0.00
//oswald_efficiency_factor=0.700
wing_winglets_flag=0
wing_sweep=0.0
wing_pos_apex_lon=-1.3
wing_pos_apex_vert=4.3
htail_area=185.461
htail_span=29.823
htail_pos_lon=-40.2
htail_pos_vert=3.000
htail_incidence=0.000
htail_sweep=21.000
vtail_area=192.4
vtail_span=16.076
vtail_sweep=25.000
vtail_pos_lon=-37.1
vtail_pos_vert=3.0
elevator_area=55.54
aileron_area=32.9375
rudder_area=53.819
elevator_up_limit=30.0 //real
elevator_down_limit=15.0 //real
aileron_up_limit=24.0 // real
aileron_down_limit=16.0 //real
rudder_limit=25.000 //real
elevator_trim_limit=20.0 //real
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

//0  Class                        <0=none,1=wheel, 2=scrape, 3=float>
//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)
oswald_efficiency_factor=0.700077
//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)

[contact_points]
static_pitch=-0.002
static_cg_height=7.0
gear_system_type=0
point.0=1.000, 19.0, 0.00, -7.00, 600, 0, 0.618, 30.000, 0.115, 2.500, 0.990, 4.000, 4.000, 0.000, 162.000, 166.000
point.1=1.000, -5.900, -12.956, -7.80, 800.0, 1.000, 0.618, 0.315, 0.799, 0.850, 0.831, 5.000, 5.000, 2.000, 162.000, 166.000
point.2=1.000, -5.900,   12.956, -7.80, 800.0, 2.000, 0.618, 0.315, 0.799, 0.850, 0.831, 5.000, 5.000, 3.000, 162.000, 166.000
point.3 =2.00, 24.33, -0.00, -4.90, 9000, 0, 0.0, 0.0, 0.00, 0.0, 0.00, 0.00, 0.00, 4, 0, 0
point.4 =2.00, -5.96, 0.00, -5.24, 6000, 0, 0.0, 0.0, 0.00, 0.0, 0.00, 0.00, 0.00, 4, 0, 0
point.5 =2.00,-44.75, 0.00, -1.00, 6000, 0, 0.0, 0.0, 0.00, 0.0, 0.00, 0.00, 0.00, 9, 0, 0
point.6 =2.00, -8.92, -47.50, 3.42, 3000, 0, 0.0, 0.0, 0.00, 0.0, 0.00, 0.00, 0.00, 5, 0, 0
point.7 =2.00, -8.92, 47.50, 3.43, 3000, 0, 0.0, 0.0, 0.00, 0.0, 0.00, 0.00, 0.00, 6, 0, 0
point.8 =2.00, -4.92, -47.50, 3.42, 3000, 0, 0.0, 0.0, 0.00, 0.0, 0.00 , 0.00, 0.00, 5, 0, 0
point.9 =2.00, -4.92, 47.50, 3.42, 3000, 0, 0.0, 0.0, 0.00, 0.0, 0.00, 0.00, 0.00, 6, 0, 0
point.10=2.00, -1.00, -12.50, -1.30, 6000, 0, 0.0, 0.0, 0.00, 0.0, 0.00, 0.00, 0.00, 5, 0, 0
point.11=2.00, -1.00, 12.50, -1.30, 6000, 0, 0.0, 0.0, 0.00, 0.0, 0.00, 0.00, 0.00, 6, 0, 0
point.12=2.00,-41.75, 0.00, 20.00, 3000, 0, 0.0, 0.0, 0.00, 0.0, 0.00, 0.00, 0.00, 8, 0, 0
point.13=2.00,-36.50, 0.00, 9.00, 3000, 0, 0.0, 0.0, 0.00, 0.0, 0.00, 0.00, 0.00, 8, 0, 0
point.14=2.00, 0.75, 0.00, 5.50, 3000, 0, 0.0, 0.0, 0.00, 0.0, 0.00, 0.00, 0.00, 7, 0, 0
point.15=2.00, 20.50, 0.00, 3.75, 3000, 0, 0.0, 0.0, 0.00, 0.0, 0.00, 0.00, 0.00, 8, 0, 0

[Flaps.0]
type=1
span-outboard=0.600
extending-time=16.000
system_type=1
damaging-speed=162.000
blowout-speed=170.000
lift_scalar=2.0
drag_scalar=0.1
pitch_scalar=1.000
flaps-position.0=0.000, 0
flaps-position.1=5.000, 162.0
flaps-position.2=10.000, 0.0
flaps-position.3=15.000, 0
flaps-position.4=20.000, 135.0
flaps-position.5=25.000, 0
flaps-position.6=30.000, 0
flaps-position.7=38.000, 0

[TailHook]
tailhook_length=4                               ;(feet)
tailhook_position = -15.0, 0.0, -1.0            ;(feet) longitudinal, lateral, vertical positions from datum
cable_force_adjust = 1.0

[folding_wings]
wing_fold_system_type=4
fold_rates=0.075,0.075

[exits]
number_of_exits = 2
exit_rate.0 = 0.09                             ;Percent per second
exit_rate.1 = 0.2                               ;Percent per second

[Reference Speeds]
flaps_up_stall_speed=102.000
full_flaps_stall_speed=82.800
cruise_speed=215.000
max_indicated_speed=292.000000
max_mach=0.650000

[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, 1
Adf.1=1
Transponder.1=1
Marker.1=1

[autopilot]
autopilot_available=0
flight_director_available=0
default_vertical_speed=1000.000000
autothrottle_available=0
autothrottle_arming_required=0
autothrottle_takeoff_ga=0
autothrottle_max_rpm=90.000000
pitch_takeoff_ga=8.000000
use_no_default_bank=0	//For no wing leveler when AP On
use_no_default_pitch=0	//For no pitch holding when AP On
autoland_available=0

[Lights]        
//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing
light.0 = 3, -5.96,-47.67, 3.24, fx_navredm ,
light.1 = 3, -5.96, 47.67, 3.24, fx_navgrem ,
light.2 = 2, -37.53,  0.00, 9.21, fx_beaconb ,
light.3 = 2, -8.50,  0.00, -4.21, fx_beaconh,
light.4 = 3, -49.50,   0.00,  4.00, fx_navwhi ,
light.5 = 4, 17, 2.0, 2.0, fx_vclight //jarkost' v cokpote
light.6 = 4, 17, -2.0, 2.0, fx_vclight //jarkost' v cokpote

//light.7 = 3, 0, -15.0, 4.3, fx_navwhi //peredn kromka
//light.8 = 3, 0, 0,-4.1, fx_navwhi // niz fusel
//light.9 = 3, 8.7, -15.0, 3.0, fx_navwhi // prop
//light.10 = 3, 19, -2.0, -6.0, fx_navwhi // per shassi
//light.11 = 3, -5.9, -15.0, -6.0, fx_navwhi //shassi

[brakes]
toe_brakes_scale=0.518815
parking_brake=1

[gear_warning_system]
gear_warning_available=0
pct_throttle_limit=0.099976
flap_limit_power=30.022988
flap_limit_idle=55.011494

[hydraulic_system]
electric_pumps=0
engine_map=1,1,0,0
normal_pressure=3000.000000

[stall_warning]
type=1

[pitot_static]
vertical_speed_time_constant=10

[attitude_indicators]
attitude_indicator.0=1

[turn_indicators]
turn_indicator.0=1,0

[keyboard_response]
elevator=150.000000,250.000000
aileron=150.000000,250.000000
rudder=150.000000,250.000000

[Views]
eyepoint=18.0, -1.76, 2.04

[direction_indicators]
direction_indicator.0=3,0

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