// Title:	An-30 dynamics
// Author:	Curl-Aless
// Version:	v4.3
// Date:	June 2005

[FLTSIM.0]
TITLE=Antonov An-30-UN
SIM=An30
MODEL=D
PANEL=
SOUND=
TEXTURE=UN
KB_CHECKLISTS=
KB_REFERENCE=
atc_id=47829
atc_airline=Aeroflot
atc_flight_number=87756
ui_manufacturer=Antonov
ui_type=An-30
ui_variation=United Nations
EDITABLE=0
description=Aerial photography aircraft. Based on An-24. Some An-30 are being employed on ecological survey missions.\nVarious camera and sensors are integrated into the fuselage.\nThis UN modification carries an external radiation measurement equipment and an external fuel tank\nFSDS Model by Samdim (c) 2003
atc_heavy=0

[FLTSIM.1]
TITLE=Antonov An-30-AER
SIM=An30
MODEL=
PANEL=
SOUND=
TEXTURE=AER
KB_CHECKLISTS=
KB_REFERENCE=
atc_id=47829
atc_airline=Aeroflot
atc_flight_number=87756
ui_manufacturer=Antonov
ui_type=An-30
ui_variation=Aeroflot
EDITABLE=0
description=Aerial photography aircraft. Based on An-24. Some An-30 are being employed on ecological survey missions.\nVarious camera and sensors are integrated into the fuselage.\n\nFSDS Model by Samdim (c) 2003
atc_heavy=0

[FLTSIM.2]
TITLE=Antonov An-30-PL
SIM=An30
MODEL=
PANEL=
SOUND=
TEXTURE=PL
KB_CHECKLISTS=
KB_REFERENCE=
atc_id=47829
atc_airline=Aeroflot
atc_flight_number=87756
ui_manufacturer=Antonov
ui_type=An-30
ui_variation=Novosibirsk Airlines
description=Aerial photography aircraft. Based on An-24. Some An-30 are being employed on ecological survey missions.\nVarious camera and sensors are integrated into the fuselage.\n\nFSDS Model by Samdim (c) 2003

[FLTSIM.3]
TITLE=Antonov An-30-Russian Air Force
SIM=An30
MODEL=
PANEL=
SOUND=
TEXTURE=RAF
KB_CHECKLISTS=
KB_REFERENCE=
atc_id=47829
atc_airline=Antonov Airlines
atc_flight_number=87752
ui_manufacturer=Antonov
ui_type=An-30
ui_variation=Russian Air Force
description=Aerial photography aircraft. Based on An-24. Some An-30 are being employed on ecological survey missions.\nVarious camera and sensors are integrated into the fuselage.\n\nFSDS Model by Samdim (c) 2003

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

// --- do not modify afer this line ---
[General]
performance=Cruise speed 460 km/h \nMTOW 23000 kg \nLength 24.3m \nWingspan 29.2m \nFirst Flight : 1973 
atc_type=Antonov
atc_model=AN30

[GeneralEngineData]
engine_type=5
Engine.0=8.3, -12.956, 3.0
Engine.1=8.3, 12.956, 3.0
fuel_flow_scalar=1.0
min_throttle_limit=0.0

[Propeller]
thrust_scalar=1.06
propeller_type=0
propeller_diameter=12.795
propeller_blades=4
propeller_moi=300
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=8.0
minimum_reverse_beta=0.0 //19.0 for LSL
rotation=1, 1

[Turboprop_engine]
power_scalar=1.1 
maximum_torque=10614.3602
max_rpm_mechanical_efficiency_scalar=1.000
idle_rpm_mechanical_efficiency_scalar=1.000
max_rpm_friction_scalar=0.7200
idle_rpm_friction_scalar=1.000

[TurbineEngineData]
fuel_flow_scalar=0.737
fuel_flow_gain=0.0030
inlet_area=1.000
rated_N2_rpm= 15100
static_thrust=625
afterburner_available=0

[flight_tuning]
cruise_lift_scalar=1.0 
pitch_stability=1.5
roll_stability=1.5
yaw_stability=1.000
parasite_drag_scalar=1.0
induced_drag_scalar=1.0
elevator_effectiveness=0.8
aileron_effectiveness=1.00
rudder_effectiveness=1.50
elevator_trim_effectiveness=0.5
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=50705.34  //23000 kg
MLW=50705.34  //23000 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=152730.00
empty_weight_pitch_MOI=244069.00
empty_weight_yaw_MOI=311215.00
empty_weight_coupled_MOI=1800.00
max_gross_weight=50705.34   //23000kg
CG_forward_limit=-2.7
CG_aft_limit=-4.32

max_number_of_stations=50
station_load.0=0.000000,-3.100000,0.000000,0.000000

[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=1100 //807.073 //- real 
wing_span=87.725 //- real
wing_root_chord=9.2
wing_dihedral=0.000
wing_incidence=0.0
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=16.0 //24.0 //real
aileron_down_limit=16.0 //real
rudder_limit=25.000 //real
elevator_trim_limit=20.0 //real
spoiler_limit=1.000
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)
//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, -7.10, 600, 0, 0.618, 58.000, 0.115, 2.500, 0.990, 4.000, 4.000, 0.000, 162.000, 166.000
point.1=1.000, -5.900, -12.956, -7.70, 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, -7.70, 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=1.9
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
light.6 = 4, 17, -2.0, 2.0, fx_vclight
light.7 = 5, -2.00, 26.42, 3.7, fx_landing ,
light.8 = 5, -2.00, -26.42, 3.7, fx_landing ,

[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=18.5, -1.70, 2.1

[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