[fltsim.0]
title=SNCASO Trident reflexive 
sim=SNCASO Trident
model=reflexive
panel=
sound=
texture=reflexive
kb_checklists=
ui_manufacturer=SNCASO
ui_type=Trident
ui_variation=1)-reflexive texture, missile and pitot
description="SNCASO SO 9050 Trident, prototype with reflexive texture, pitot and missile - Designer P. Grange, Paris, April 2007"

[fltsim.1]
title=SNCASO Trident ref pitot 
sim=SNCASO Trident
model=refpit
panel=
sound=
texture=reflexive
kb_checklists=
ui_manufacturer=SNCASO
ui_type=Trident
ui_variation=2)-reflexive texture, pitot no missile
description="SNCASO SO 9050 Trident, prototype with reflexive texture, pitot no missile - Designer P. Grange, Paris, April 2007"

[fltsim.2]
title=SNCASO Trident ref missile 
sim=SNCASO Trident
model=refmiss
panel=
sound=
texture=reflexive
kb_checklists=
ui_manufacturer=SNCASO
ui_type=Trident
ui_variation=3)-reflexive texture, missile no pitot
description="SNCASO SO 9050 Trident, prototype with reflexive texture, missile no pitot - Designer P. Grange, Paris, April 2007"

[fltsim.3]
title=SNCASO Trident camo 
sim=SNCASO Trident
model=camo
panel=
sound=
texture=camo
kb_checklists=
ui_manufacturer=SNCASO
ui_type=Trident
ui_variation=4)-fictional camo and weapons, sand
description="If the SNCASO Trident had been chosen by the Air Force instead of the Mirage, the beast would have looked like that ... Let's rewrite the history just for the fun ! - Designer P. Grange, Paris, April 2007"

[fltsim.4]
title=SNCASO Trident camo2 
sim=SNCASO Trident
model=camo
panel=
sound=
texture=camo2
kb_checklists=
ui_manufacturer=SNCASO
ui_type=Trident
ui_variation=5)-fictional camo and weapons, green
description="If the SNCASO Trident had been chosen by the Air Force instead of the Mirage, the beast would have looked like that ... Let's rewrite the history just for the fun ! - Designer P. Grange, Paris, April 2007"


[fltsim.5]
title=SNCASO Trident clean
sim=SNCASO Trident
model=clean
panel=
sound=
texture=clean
kb_checklists=
ui_manufacturer=SNCASO
ui_type=Trident
ui_variation=6)-matt grey, clean, with nose pitot tube
description="SNCASO SO 9050 Trident, - Designer P. Grange, Paris, April 2007"

[fltsim.6]
title=SNCASO Trident missile
sim=SNCASO Trident
model=missi
panel=
sound=
texture=missi
kb_checklists=
ui_manufacturer=SNCASO
ui_type=Trident
ui_variation=7)-matt grey, missile, no nose pitot tube
description="SNCASO SO 9050 Trident, - Designer P. Grange, Paris, April 2007"


[General]
atc_type=SNCASO 
atc_model=Trident 
editable=0 
performance=Span: 6.98 m\nLength: 12.70 m\nWeight: 2,625 kg empty, 5,150 kg gross\nSpeed: 2,000 km/h\nCeiling: 25,000 m\nPower: 2 x 745 kgp Dassault MD-30 'Viper' + 1 rocket SEPR 631, 3000 kgp 

[weight_and_balance]

// ACM V2.3
max_gross_weight = 41537
empty_weight = 22696
reference_datum_position = 0, 0, 0
empty_weight_CG_position = 0, 0, 0
empty_weight_pitch_MOI = 196385
empty_weight_roll_MOI = 175000
empty_weight_yaw_MOI = 250000
empty_weight_coupled_MOI = 1300
max_number_of_stations = 1

station_load.0 = 0.000000,0.000000,0.000000,0.000000


[lights]

//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing

light.0 = 3,  1.0, -11.89,  1.07, fx_navred ,
light.1 = 3,  1.0,  11.89,  1.07, fx_navgre ,
light.2 = 3, -16.28,   0.0,  7.41, fx_navwhi ,
light.3 = 4,  11.78,  0.00, 1.38, fx_vclight ,
light.4 = 9, -6.0, -10.29, 1.18, Trident_Moteur ,
light.5 = 9, -6.0, 10.29, 1.18, Trident_Moteur
light.6 = 5, -21.3, 0.0, 0.39, fx_burner2

[GeneralEngineData]

//0=Piston, 1=Jet, 2=None, 3=Helo-Turbine, 4=Rocket, 5=Turboprop
engine_type = 1
fuel_flow_scalar = 1.000000
engine.0 = 0.000000,0.000000,0.000000
min_throttle_limit=0.100000

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

[fuel]

//Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)

fuel_type = 2
number_of_tank_selectors = 1

Center1 = 0, 0, 0, 300, 0
Center2 = 0, 0, 0, 300, 0
LeftMain = 0, 0, 0, 300, 0
RightMain = 0, 0, 0, 300, 0
electric_pump=0


[contact_points]
static_pitch = 0.6
static_cg_height = 5
max_number_of_points = 8

point.0 = 1, 13.044, 0, -5.9776, 1181.102, 0, 0.79, 22, 0.946, 1.22, 0.441, 2, 3, 0, 0, 0
point.1 = 1, -3.6122, -4.1637, -6.4964, 1574.803, 1, 0.632, 0, 1.867, 1.7, 0.744, 2, 3, 2, 0, 0
point.2 = 1, -3.4558, 4.1623, -6.515, 1574.803, 2, 0.632, 0, 1.867, 1.7, 0.744, 2, 3, 3, 0, 0
point.3 = 2, -7.591, -18.1709, -1.2697, 787.402, 0, 0, 0, 0, 0, 0, 0, 0, 5, 0, 0
point.4 = 2, -7.591, 18.0417, -1.2697, 787.402, 0, 0, 0, 0, 0, 0, 0, 0, 6, 0, 0
point.5 = 2, -23.8931, 0, -2.2113, 787.402, 0, 0, 0, 0, 0, 0, 0, 0, 9, 0, 0
point.6 = 2, 31.0695, 0, -0.6495, 787.402, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0
point.7 = 5.000, 13.192, 0.000, -6.300, 1600, 0, 0.00, 50.0, 0.0,  0.0, 1.00, 3.0, 3.0, 0, 0.0, 0.0
gear_system_type=0


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


[forcefeedback]
gear_bump_nose_magnitude = 6000
gear_bump_nose_direction = 18000
gear_bump_nose_duration = 250000
gear_bump_left_magnitude = 6000
gear_bump_left_direction = 35500
gear_bump_left_duration = 250000
gear_bump_right_magnitude = 6000
gear_bump_right_direction = 00500
gear_bump_right_duration = 250000
ground_bumps_magnitude1 = 3250
ground_bumps_angle1 = 8900
ground_bumps_intercept1 = 5.0
ground_bumps_slope1 = 0.48
ground_bumps_magnitude2 = 750
ground_bumps_angle2 = 9100
ground_bumps_intercept2 = 0.075
ground_bumps_slope2 = 1.0
crash_magnitude1 = 10000
crash_direction1 = 01000
crash_magnitude2 = 10000
crash_direction2 = 9000
crash_period2 = 75000
crash_duration2 = 2500000

[airplane_geometry]

wing_area = 376.000000
wing_span = 36.66
wing_root_chord = 10.833333
wing_dihedral = 1.0
wing_incidence = -0.494385
wing_twist = 0.351563
oswald_efficiency_factor = 3.195582
wing_winglets_flag = 0
wing_sweep = 0.000000
wing_pos_apex_lon = 0.000000
wing_pos_apex_vert = 0.000000
htail_area = 230.000000
htail_span = 22.50000
htail_pos_lon = -17.10000
htail_pos_vert = 0.000000
htail_incidence = 0.000000
htail_sweep = 0.000000
vtail_area = 88.000000
vtail_span = 11.000
vtail_sweep = 0.000000
vtail_pos_lon = -17.33333
vtail_pos_vert = 6.333333
elevator_area = 50.000000
aileron_area = 16.080000
rudder_area = 88.000000
elevator_up_limit = 11.0
elevator_down_limit = 11.0
aileron_up_limit = 22.0
aileron_down_limit = 22.0
rudder_limit = 22.0
elevator_trim_limit = 19.480565
spoiler_limit = 59.988681
aileron_to_spoileron_gain = 0.000000
min_ailerons_for_spoilerons = 0.000000
min_flaps_for_spoilerons = 0.000000
spoilerons_available = 0

[electrical]
max_battery_voltage = 24
generator_alternator_voltage = 28
max_generator_alternator_amps = 60
electric_always_available = 0

[flight_tuning]
elevator_effectiveness=1.3 
aileron_effectiveness=0.8 
rudder_effectiveness=1.0 

[Flaps.0]
type=1
span-outboard=0.500000
extending-time=4.000000
system_type=0
flaps-position.0=0.000000,0.000000
flaps-position.1=13.330818,0.000000
flaps-position.2=26.661636,0.000000
flaps-position.3=39.992454,0.000000

[TurbineEngineData]
fuel_flow_gain=0.002500 
inlet_area=16.289500 
rated_N2_rpm=29920.000000 
static_thrust=17200.000000 
afterburner_available=1 
reverser_available=0 

[jet_engine]
thrust_scalar=1.30

[Reference Speeds]
flaps_up_stall_speed=145.000000 
full_flaps_stall_speed=116.000000 
cruise_speed=380.786348 
max_indicated_speed=810.000000
max_mach=2.500000

[Views]
eyepoint=18.5, 0, 3.14 

[autopilot]
autopilot_available=1 
flight_director_available=1 
default_vertical_speed=4800.000000 
autothrottle_available=1 
autothrottle_arming_required=0
autothrottle_takeoff_ga=0
autothrottle_max_rpm=110.000000
pitch_takeoff_ga=8.000000 
max_pitch=10.000000
max_pitch_acceleration=1.000000
max_pitch_velocity_lo_alt=2.000000
max_pitch_velocity_hi_alt=1.500000
max_pitch_velocity_lo_alt_breakpoint=20000.000000
max_pitch_velocity_hi_alt_breakpoint=28000.000000
max_bank=25.000000
max_bank_acceleration=1.800000
max_bank_velocity=3.000000
max_throttle_rate=0.100000
nav_proportional_control=9.000000
nav_integrator_control=0.250000
nav_derivative_control=0.000000
nav_integrator_boundary=2.500000
nav_derivative_boundary=0.000000
gs_proportional_control=9.520000
gs_integrator_control=0.260000
gs_derivative_control=0.000000
gs_integrator_boundary=0.700000
gs_derivative_boundary=0.000000
yaw_damper_gain=0.000000

[direction_indicators]
direction_indicator.0=3,0 

[brakes]
toe_brakes_scale=1.000031
parking_brake=1
[hydraulic_system]
electric_pumps=0
engine_map=1,1,0,0
normal_pressure=3000.000000
[stall_warning]
type=1
[attitude_indicators]
attitude_indicator.0=1
[turn_indicators]
turn_indicator.0=1,0
[folding_wings]
wing_fold_system_type=4                       ;0=None
fold_rates=0.12,0.11                          ;Percent per second
[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
[exits]
number_of_exits = 2 
exit_rate.1 = 0.4                               ;Percent per second 
exit_rate.0 = 0.4                               ;Percent per second

[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 

[gear_warning_system]
gear_warning_available=0
pct_throttle_limit=0.000000
flap_limit_power=0.000000
flap_limit_idle=0.000000