[fltsim.0]
title=RFN Rafale
sim=RFN Rafale
model=
panel=
sound=
texture=
kb_checklists=
kb_reference=
atc_id=N°5
atc_airline=Aéronavale
atc_flight_number=
atc_heavy=1
ui_manufacturer=Dassault Aviation
ui_type=Rafale Marine
ui_variation=RFN Flottille 12F n°5
description=Rafale Marine RFN  -Royale French Navy-\n  http:\/\/sonny3.free.fr\nOriginal aircraft by Christophe Rosenmann\n  razorback@hydromail.com\nNew paint Flotille 12F by Y-Raymond\nOriginal panel by Oxyd\n  oxyd@nytrium.net\nfictional adaptation panel by Y-Raymond\nFichier AIR by Benoit M. Dubé\n  dube_benoit_m@yahoo.fr\nversion b5\n2002 fevrier 25



[jet_engine]
thrust_scalar=1

[exits]
number_of_exits=1
exit_rate.0=0.4  				;Percent per second

[TailHook]
tailhook_length=4				;(feet)
tailhook_position=-23.6, 0.0, -1.0		;(feet) longitudinal, lateral, vertical positions from datum
cable_force_adjust=1.0

[electrical]
max_battery_voltage=24.0
generator_alternator_voltage=28.0
max_generator_alternator_amps=60.0

[contact_points]
//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

point.0=1,   9.30,  0.0, -8.88, 2362,   0, 1.2, 30, 0.972362, 2.5, 0.710573, 5, 5, 0
point.1=1,  -8.38, -4.77,-7.37, 2362,   1, 1.6,  0, 0.316353, 2.5, 1.112804, 5, 5, 2
point.2=1,  -8.38,  4.77,-7.37, 2362,   2, 1.6,  0, 0.316353, 2.5, 1.112804, 4, 4, 3
point.3=2,  -9.92,-13.92,-1.67, 1574.8, 0,   0,  0,        0,   0,        0, 0, 0, 5
point.4=2,  -9.92, 13.92,-1.67, 1574.8, 0,   0,  0,        0,   0,        0, 0, 0, 6
point.5=2, -17.58,     0,-3.67, 1574.8, 0,   0,  0,        0,   0,        0, 0, 0, 9
point.6=2,  16.67,     0,-3.67, 1574.8, 0,   0,  0,        0,   0,        0, 0, 0, 4
static_pitch=3.368		//degrees (pitch when loaded on ground)
static_cg_height=8.127	//(feet) altitude of CG when at rest (altitude when loaded on ground)

[Views]
eyepoint=10.720668,0.000000,4.521998

[General]
performance=Power:2 Snecma M88-2@17000 lb\afterburners\nRange: 750 (combat radius)\n

[WEIGHT_AND_BALANCE]
reference_datum_position=0.000000,0.000000,0.000000
empty_weight_CG_position=0.000000,0.000000,0.000000
max_number_of_stations=50
station_load.0=0.000000,0.000000,0.000000,0.000000
empty_weight=23000.000000
empty_weight_roll_MOI=298163.000000
empty_weight_pitch_MOI=270200.000000
empty_weight_yaw_MOI=455000.000000
empty_weight_coupled_MOI=1300.000000

[fuel]
Center1=0.000000,0.000000,0.000000,1552.000000,0.000000
fuel_type=2.000000
number_of_tank_selectors=1

[airplane_geometry]
wing_area=482.000000
wing_span=45.000000
wing_root_chord=10.750000
wing_dihedral=2.999268
wing_incidence=0.000000
wing_twist=0.000000
oswald_efficiency_factor=82.756253
wing_winglets_flag=0
wing_sweep=0.000000
wing_pos_apex_lon=0.000000
wing_pos_apex_vert=0.000000
htail_area=110.000000
htail_span=22.083333
htail_pos_lon=-23.333333
htail_pos_vert=0.000000
htail_incidence=0.000000
htail_sweep=0.000000
vtail_area=100.000000
vtail_span=11.401754
vtail_sweep=0.000000
vtail_pos_lon=-20.000000
vtail_pos_vert=0.000000
elevator_area=20.000000
aileron_area=21.000000
rudder_area=10.200000
elevator_up_limit=27.501974
elevator_down_limit=20.626481
aileron_up_limit=19.480565
aileron_down_limit=14.896903
rudder_limit=23.491270
elevator_trim_limit=19.480565
spoiler_limit=59.988681
spoilerons_available=0
aileron_to_spoileron_gain=0.000000
min_ailerons_for_spoilerons=0.000000
min_flaps_for_spoilerons=0.000000

[Flaps.0]
type=1
span-outboard=0.500000
extending-time=5.000000
system_type=0
flaps-position.0=0.000000,0.000000
flaps-position.1=19.996227,0.000000
flaps-position.2=39.992454,0.000000

[GeneralEngineData]
engine_type=1
Engine.0=-13.333333,-1.666667,0.000000
Engine.1=-13.333333,1.666667,0.000000
fuel_flow_scalar=1.000000

[TurbineEngineData]
fuel_flow_gain=0.002170
inlet_area=19.251240
rated_N2_rpm=29920.000000
static_thrust=16042.700000
afterburner_available=1
reverser_available=1

[Reference Speeds]
flaps_up_stall_speed=120.000000
full_flaps_stall_speed=96.000000
cruise_speed=985.182215

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

[SMOKESYSTEM]
smoke.0=-5.00, -30.00, 5.00,  fx_smoke_RFN
smoke.1=-5.00, -30.00, 3.00,  fx_smoke_RFN
smoke.2=-5.00, -30.00, -5.00,  fx_smoke_RFN
smoke.3=-5.00, -30.00, -3.00,  fx_smoke_RFN

[EFFECTS]
wake=fx_wake
/water=fx_spray
water=fx_waterland
dirt=fx_tchdrt
concrete=fx_sparks
;touchdown=fx_tchdwn_s, 1

[autopilot]
autopilot_available=1
flight_director_available=0
default_vertical_speed=1800.000000
autothrottle_available=1
autothrottle_arming_required=0
autothrottle_takeoff_ga=0
autothrottle_max_rpm=90.000000
pitch_takeoff_ga=8.000000

[direction_indicators]
direction_indicator.0=3,0