[fltsim.0]
title=Hispano Aviación HA200 Saeta  
sim=HA200
model=se
panel=
sound=
texture=gue
kb_checklists=
kb_reference=
atc_id=
ui_manufacturer=España
ui_type=caza
ui_variation=HA200 Saeta  FIO
visual_damage=1
description=History: The jet-engined, straight wing Saeta ("Arrow") was built by Hispano under the direct guidance of famed designer Willy Messerschmitt. First flown on 12 August 1955, it was built as both a basic trainer (HA-200A with two pilots in tandem) and as a light attack aircraft (HA-220, pilot only, equipped with two underwing weapons pylons and two 7.62mm machine-guns). Thirty "A"-models were delivered to the Spanish air force, which was anxious to end reliance on foreign imports (principally the T-6 Texan) in the early 1960's. The Spanish Air Force designated the trainer the E.14 and the attack version the C.10. In 1965, Hispano installed the more powerful Marbore VI engine and designated this variant the HA-200D. It was so successful that they added armor, doubled the number of underbody hard points and fitted Browning M3 machine guns, resulting in a specialized version called the HA-200E Super Saeta. This plane saw active service in the Sahara in 1974-75. 
atc_heavy=0
atc_airline=
atc_flight_number=

[fltsim.1]
title=Hispano Aviación Saeta  
sim=HA200
model=pr
panel=
sound=
texture=esc
kb_checklists=
kb_reference=
atc_id=
ui_manufacturer=España
ui_type=entrenamiento
ui_variation=HA200 Saeta  FIO
visual_damage=1
description=History: The jet-engined, straight wing Saeta ("Arrow") was built by Hispano under the direct guidance of famed designer Willy Messerschmitt. First flown on 12 August 1955, it was built as both a basic trainer (HA-200A with two pilots in tandem) and as a light attack aircraft (HA-220, pilot only, equipped with two underwing weapons pylons and two 7.62mm machine-guns). Thirty "A"-models were delivered to the Spanish air force, which was anxious to end reliance on foreign imports (principally the T-6 Texan) in the early 1960's. The Spanish Air Force designated the trainer the E.14 and the attack version the C.10. In 1965, Hispano installed the more powerful Marbore VI engine and designated this variant the HA-200D. It was so successful that they added armor, doubled the number of underbody hard points and fitted Browning M3 machine guns, resulting in a specialized version called the HA-200E Super Saeta. This plane saw active service in the Sahara in 1974-75. 
atc_heavy=0
atc_airline=
atc_flight_number=

[General]
atc_type=
atc_model=
performance=Engines: \t02 Turbomeca Marbore VI turbojets. \nWeight: \tEmpty 4,453 lbs. , Max Takeoff\t 7,937 lbs.\nWing Span: \t34ft., 1.75 in.\nLength: \t29ft. 5in. \nHeight: \t9ft. 4.25in.\nMax. Speed: \t430 mph. \nCeiling: \t42,650 ft.\nRange: \t930 miles\nArmament: \tTwo 7,7 mm mahine guns in nose + underwing hardpoints for a variety of weapons\n


[WEIGHT_AND_BALANCE]
max_gross_weight = 20450.000
empty_weight = 11700.000

reference_datum_position     = 34.500, 0.000, 0.000
empty_weight_CG_position     = -35.790, 0.000, 0.000

max_number_of_stations = 50

station_load.0  = 170.000, -17.000, -1.200, 0.000
station_load.1  = 170.000, -17.000, 1.200, 0.000
station_load.2  = 170.000, -22.500, -1.200, 0.000
station_load.3  = 170.000, -22.500, 1.200, 0.000
station_load.4  = 170.000, -26.700, -1.200, 0.000
station_load.5  = 170.000, -26.700, 1.200, 0.000
station_load.6  = 170.000, -30.900, -1.200, 0.000
station_load.7  = 170.000, -30.900, 1.200, 0.000
station_load.8  = 170.000, -35.100, -1.200, 0.000
station_load.9  = 170.000, -35.100, 1.200, 0.000
station_load.10 = 100.000, -42.000, 0.000, 0.000
station_load.11 = 50.000, -45.000, 0.000, 0.000


;Moments of Inertia
empty_weight_pitch_MOI   = 50000.000
empty_weight_roll_MOI    = 45000.000
empty_weight_yaw_MOI     = 70000.000
empty_weight_coupled_MOI = 0.000
CG_forward_limit= 0.000
CG_aft_limit= 1.000

[electrical]
max_battery_voltage = 12.0
generator_alternator_voltage = 13.8
max_generator_alternator_amps = 40.0

                ;BusType, MaxAmpLoad, MinVoltage       BusTypes:0=MainBus,1=AvionicsBus,2=BatteryBus,3=HotBatteryBus,4-7=Generator/AlternatorBus(1-4)
avionics_bus       = 0, 10, 9.5
avionics           = 1, 5 , 9.5
additional_system  = 0, 20, 9.5
marker_beacon      = 1, 2 , 9.0
fuel_pump          = 0, 5 , 9.0

[flight_tuning]
cruise_lift_scalar     = 1.0
parasite_drag_scalar   = 1.0
induced_drag_scalar    = 1.0
elevator_effectiveness = 1.0
aileron_effectiveness  = 3.0
rudder_effectiveness   = 1.0
pitch_stability        = 1.0
roll_stability         = 1.0
yaw_stability          = 1.0
elevator_trim_effectiveness = 1.0
aileron_trim_effectiveness  = 1.0
rudder_trim_effectiveness   = 1.0

[GeneralEngineData]
engine_type = 1
Engine.0 = -42.800, -4.800, 0.800
Engine.1 = -42.800, 4.800, 0.800
fuel_flow_scalar        = 1.000

[TurbineEngineData]
fuel_flow_gain          = 0.003
inlet_area              = 4.290
rated_N2_rpm            = 29920.000
static_thrust           = 3500.000
afterburner_available   = 0
reverser_available      = 1

[jet_engine]
thrust_scalar = 1.0


        //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]
point.0= 1.000, -11.170, 0.000, -4.920, 1181.100, 0.000, 0.635, 46.800, 0.420, 2.500, 0.588, 10.000, 10.000, 0.000, 0.000, 0.000
point.1= 1.000, -37.250, -4.750, -5.320, 1574.800, 1.000, 0.635, 0.000, 0.480, 2.500, 0.546, 9.000, 9.000, 2.000, 0.000, 0.000
point.2= 1.000, -37.250, 4.750, -5.320, 1574.800, 2.000, 0.635, 0.000, 0.480, 2.500, 0.546, 9.000, 9.000, 3.000, 0.000, 0.000
point.3= 2.000, -37.830, -23.920, -3.000, 787.400, 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, -37.830, 23.920, -3.000, 787.400, 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, -57.170, 0.000, 0.000, 787.400, 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, -11.470, 0.000, -1.500, 787.400, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 4.000, 0.000, 0.000

static_pitch = -0.750
static_cg_height = 4.410

[Views]
eyepoint = -33.20, 00.00, 2.00



[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, 0
Adf.1         = 1
Transponder.1 = 1
Marker.1      = 1

[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 = 150, 250
aileron  = 150, 250
rudder   = 150, 250

[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=3,0

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

[fuel]
Center1   = -41.400, 0.000, -1.500, 359.000, 0.000
LeftMain  = -36.300, -10.000, -1.500, 268.500, 0.000
RightMain = -36.300, 10.000, -1.500, 268.500, 0.000
fuel_type = 2                                   //Fuel type: 1 = Avgas, 2 = JetA
number_of_tank_selectors = 1

[airplane_geometry]
wing_area               = 312.000
wing_span               = 45.800
wing_root_chord         = 7.300
wing_dihedral           = 2.500
wing_incidence          = 0.500
wing_twist              = -1.500
oswald_efficiency_factor= 0.800
wing_winglets_flag      = 1
wing_sweep              = 35.000
wing_pos_apex_lon       = -28.000
wing_pos_apex_vert      = 0.000
htail_area              = 67.000
htail_span              = 17.200
htail_pos_lon           = -59.100
htail_pos_vert          = 0.000
htail_incidence         = 2.000
htail_sweep             = 25.000
vtail_area              = 42.000
vtail_span              = 7.400
vtail_sweep             = 30.000
vtail_pos_lon           = -55.000
vtail_pos_vert          = 4.100
elevator_area           = 17.000
aileron_area            = 13.500
rudder_area             = 7.300
elevator_up_limit       = 17.000
elevator_down_limit     = 15.500
aileron_up_limit        = 18.000
aileron_down_limit      = 18.000
rudder_limit            = 30.000
elevator_trim_limit     = 15.000
spoiler_limit           = 60.000
spoilerons_available    = 0
aileron_to_spoileron_gain = 4.600
min_ailerons_for_spoilerons = 5.000
min_flaps_for_spoilerons= 0.000

[Reference Speeds]
flaps_up_stall_speed    = 112.000
full_flaps_stall_speed  = 102.000
cruise_speed            = 564.000

[autopilot]
autopilot_available= 1
flight_director_available= 1
default_vertical_speed= 1800.0
autothrottle_available= 1
autothrottle_arming_required= 0
autothrottle_max_rpm = 90
autothrottle_takeoff_ga= 0
pitch_takeoff_ga = 8;

[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

[Flaps.0]
type= 1
span-outboard= 0.800
extending-time= 5.000
system_type= 0
damaging-speed= 250.000
blowout-speed= 300.000
lift_scalar= 1.000
drag_scalar= 1.000
pitch_scalar= 1.000
flaps-position.0= 0.000, 0.000
flaps-position.1= 8.000, 0.000
flaps-position.2= 20.000, 0.000
flaps-position.3= 40.000, 0.000