[fltsim.0]
title=Thruster
sim=Thruster
model=
panel=
sound=
texture=
kb_checklists=
description=Notes:Thruster T600 Spint (9H-UMD).Original aircraft used for flight instruction by.Island Microlight Club in Malta.\nwww.islandmicrolightclub.com\n\nCopyright:b.warwick1@ntlworld.com  June  2004\n\n

Wing Span: 9.6m (31' 6")
Wing Chord: 1.555m (5' 1.25")
Wing Area: 14.937m² (160.78ft²)
Projected lift strut area: 0.758m² (8.159ft²)
Wing reference area: 15.695m² (168.94ft²)
Overall height (top of fin): 2.41m (7' 11")
Tail plane span: 2.667m (8' 9")
Tail plane + elevator area: 2.20m² (23.68ft²)
Fin Span: 1.397m (4' 7")
Fin and Rudder area: 1.30m² (13.99ft²)

Engine
Max RPM: 3300
Max RPM continuous: 3300
Max CHT climb: 175deg C (348deg F)
Rec CHT cruise: 150deg C (320deg F)
Oil Pressure Max: 525kPa (76psi)
Oil Pressure Min: 220kPa (31psi)
Oil Temp Max: 118deg C (224deg F)
Oil Temp Min: 15deg C (59deg F)
Oil Temp Continuous: 80 - 100deg C (176 - 212deg F)

Airspeeds
Va 71Kts ( c ) 60Kts(a) and (b) IAS
Vne 102kts( c ) 80Kts(a) and (b) IAS
VC 82Kts ( c ) 76Kts(a) and (b) IAS
(Cockpit a: Open, b: Enclosed Rear, c: Enclosed rear Fusleage)

Flight Instruments:
Airspeed Indicator 0 - 140kts
Altimeter 1 - 20,000ft
Slip Indicator
Compass 

Engine Instruments
Engine Speed Indicator 0 - 4000rpm
Oil Temperature Gauge
Cylinder Head Temperature Gauge
Oil Pressure Gauge

Stalling speeds:

Stall speed varies with both aircraft weight and the manoeuvre "g" which is related to the angle of bank in a steady turn. At 450kg stall speed in kt IAS is:

Bank Angle 0deg: Vs=35
Bank Angle 20deg: Vs=37
Bank Angle 40deg: Vs=46
Bank Angle 60deg: Vs=70

Glide Performance:

At 450kg, power off, at 45kts, the horizontal distance covered during descent through 1000ft in still air has been measured at 1.13NM
ui_manufacturer=Thruster aircraft
ui_type=
ui_variation=Pilot In Command
atc_heavy=0
atc_id=9H-UMD
atc_airline=
atc_flight_number=

[Views]
eyepoint= 0.45, -0.94, 1.33        //(feet) longitudinal, lateral, vertical distance from reference datum
[General]
performance=Airspeeds\nVa 71Kts ( c ) 60Kts(a) and (b) IAS\nVne 102kts( c ) 80Kts(a) and (b) IAS\nVC 82Kts ( c ) 76Kts(a) and (b) IAS\n\n
atc_type=
atc_model=
TBAirCraftFolderUId=22

[WEIGHT_AND_BALANCE]
reference_datum_position     =  0.0000, 0.0000, 0.0000       // (feet) distance from FlightSim Reference position: (1/4 chord, centerline, waterline)

empty_weight_CG_position= -0.500, 0.000, 0.000
max_number_of_stations=50
station_load.0=0.000000,0.000000,0.000000,0.000000
empty_weight= 450.000
empty_weight_roll_MOI= 500.000
empty_weight_pitch_MOI= 500.000
empty_weight_yaw_MOI= 600.000
empty_weight_coupled_MOI= 0.000
max_gross_weight= 658.000
CG_forward_limit= 0.000
CG_aft_limit= 1.000

[fuel]
LeftMain= 0.000, 0.000, 0.000, 10.000, 0.000
RightMain= 0.000, 0.000, 0.000, 10.000, 0.000
fuel_type=1.000000
number_of_tank_selectors=1
electric_pump=1

[airplane_geometry]
wing_area= 160.780
wing_span= 31.500
wing_root_chord= 5.125
wing_dihedral= 1.000
wing_incidence= 2.500
wing_twist= -1.000
oswald_efficiency_factor= 0.751
wing_winglets_flag= 0
wing_sweep= 0.000
wing_pos_apex_lon= 0.000
wing_pos_apex_vert= 0.000
htail_area= 40.000
htail_span= 11.667
htail_pos_lon= -12.500
htail_pos_vert= 0.000
htail_incidence= 0.000
htail_sweep= 0.000
vtail_area= 23.000
vtail_span= 5.468
vtail_sweep= 0.000
vtail_pos_lon= -12.583
vtail_pos_vert= 1.500
elevator_area= 24.500
aileron_area= 44.200
rudder_area= 14.100
elevator_up_limit= 15.500
elevator_down_limit= 15.500
aileron_up_limit= 20.000
aileron_down_limit= 10.000
rudder_limit= 25.000
elevator_trim_limit= 15.000
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

[forcefeedback]
gear_bump_nose_magnitude=8000           ; 0 - 10000
gear_bump_nose_direction=18000          ; 0 - 35999 degrees
gear_bump_nose_duration=250000          ; in microseconds
gear_bump_left_magnitude=8000           ; 0 - 10000
gear_bump_left_direction=35500          ; 0 - 35999 degrees
gear_bump_left_duration=250000          ; in microseconds
gear_bump_right_magnitude=8000          ; 0 - 10000
gear_bump_right_direction=00500         ; 0 - 35999 degrees
gear_bump_right_duration=250000         ; in microseconds
ground_bumps_magnitude1=3250            ; 0 - 10000
ground_bumps_angle1=8900                ; 0 - 35999 degrees
ground_bumps_intercept1=5.0
ground_bumps_slope1=0.48
ground_bumps_magnitude2=750             ; 0 - 10000
ground_bumps_angle2=9100                ; 0 - 35999 degrees
ground_bumps_intercept2=0.075
ground_bumps_slope2=1.0
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


[contact_points]
point.0= 1.000, 3.833, 0.000, -3.083, 1574.803, 0.000, 0.504, 45.000, 0.235, 2.500, 0.729, 0.000, 0.000, 0.000, 0.000, 0.000
point.1= 1.000, -1.600, -3.100, -3.083, 1574.803, 1.000, 0.504, 0.000, 0.236, 2.500, 0.728, 0.000, 0.000, 2.000, 0.000, 0.000
point.2= 1.000, -1.600, 3.100, -3.083, 1574.803, 2.000, 0.504, 0.000, 0.236, 2.500, 0.728, 0.000, 0.000, 3.000, 0.000, 0.000
point.3= 2.000, 0.333, -14.417, 2.833, 1574.803, 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, 0.333, 14.417, 2.833, 1574.803, 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, -15.333, 0.000, -0.500, 1574.803, 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, 3.833, 0.000, -0.500, 1574.803, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 4.000, 0.000, 0.000

static_pitch= -0.083
static_cg_height= 2.851

[GeneralEngineData]
engine_type= 0
Engine.0= 10.417, 0.000, 0.417
fuel_flow_scalar= 1.000
min_throttle_limit=0.000000

[piston_engine]
max_rpm_mechanical_efficiency_scalar=1.05
idle_rpm_mechanical_efficiency_scalar=1.000
max_rpm_friction_scalar=0.850
idle_rpm_friction_scalar=1.000
cylinder_displacement= 64.000
compression_ratio= 7.000
number_of_cylinders= 4
max_rated_rpm= 3300.000
max_rated_hp= 23.763
fuel_metering_type= 2
cooling_type= 1
normalized_starter_torque= 0.300
turbocharged= 0
max_design_mp= 0.000
min_design_mp= 0.000
critical_altitude= 0.000
emergency_boost_type= 0
emergency_boost_mp_offset= 0.000
emergency_boost_gain_offset= 0.000
fuel_air_auto_mixture= 0
auto_ignition=0
power_scalar=1.000

[propeller]
propeller_type= 1
propeller_diameter= 4.500
propeller_blades= 2
propeller_moi= 2.188
beta_max= 5.565
beta_min= 15.000
min_gov_rpm= 800.000
prop_tc= 0.100
gear_reduction_ratio= 1.000
fixed_pitch_beta= 18.000
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= 0.000
minimum_on_ground_beta= 0.000
minimum_reverse_beta= 0.000
thrust_scalar=0.590

[lights]
//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit            
light.0=3,  2.75, -16.50, 3.85, fx_navred
light.1=3,  2.75,  16.50, 3.85, fx_navgre
light.2=3, -14.80,  0.00, 0.95,  fx_navwhi 
light.3=2,  2.83, -16.50, 3.85, fx_strobe
light.4=2,  2.83,  16.50, 3.85, fx_strobe
light.5=1, -14.00,  0.00, 5.90, fx_beacon
light.6=4,  2.75,   0.00, 1.85, fx_vclight


[Reference Speeds]
flaps_up_stall_speed= 30.000
full_flaps_stall_speed= 24.000
cruise_speed= 55.857
max_indicated_speed=125.007813

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

[autopilot]
autopilot_available=0
flight_director_available=0

[direction_indicators]
direction_indicator.0=1,0

[flight_tuning]
cruise_lift_scalar=1.200
pitch_stability=1.000
roll_stability=1.000
yaw_stability=1.000
parasite_drag_scalar=1.200
induced_drag_scalar=1.500
elevator_effectiveness=1.500
aileron_effectiveness=2.000
rudder_effectiveness=1.000
elevator_trim_effectiveness=1.200
aileron_trim_effectiveness=1.200
rudder_trim_effectiveness=1.000

[brakes]
toe_brakes_scale=1.200
parking_brake=1

[hydraulic_system]
normal_pressure=0.000000

[stall_warning]
type=1

[attitude_indicators]
attitude_indicator.0=1

[turn_indicators]
turn_indicator.0=1,0

[Flaps.0]
type= 0
span-outboard= 0.000
extending-time= 0.100
system_type= 0
damaging-speed= 0.000
blowout-speed= 0.000
lift_scalar= 0.000
drag_scalar= 0.000
pitch_scalar= 0.000