[fltsim.0]
title=RFN CRUSADER 14F-n°03
sim=F8ECrusader
model=
panel=
sound=
texture=14F-n°03
kb_checklists=f8e(fn)_check
kb_reference=f8e(fn)_ref
ui_manufacturer=Vought
ui_type=Crusader French Navy
ui_variation=Flottille 14F-n°03
visual_damage=1
description=Design and COPYRIGHT:     Bernd Drefahl, GER\ne-mail: bernd.drefahl@t-online.de\n\nThe Chance Vought F8 Crusader  was a carrier based super sonic air superiority fighter. The first flight was in March 1955.  With its high speed and ability to perform at above 95% of the earths atmosphere it was designed for defense against a Mach-2 bomber. \nIt had a tilting 2 position wing providing for carrier use. \n\nFichier AIR\nBenoit M. Dubé\ndube_benoit_m@yahoo.fr\n\nversion bf3\n2002 mai 17

[fltsim.1]
title=RFN CRUSADER 12F-n°10
sim=F8ECrusader
model=
panel=
sound=
texture=12F-n°10
kb_checklists=f8e(fn)_check
kb_reference=f8e(fn)_ref
ui_manufacturer=Vought
ui_type=Crusader French Navy
ui_variation=Flottille 12F-n°10
visual_damage=1
description=Design and COPYRIGHT:     Bernd Drefahl, GER\ne-mail: bernd.drefahl@t-online.de\n\nThe Chance Vought F8 Crusader  was a carrier based super sonic air superiority fighter. The first flight was in March 1955.  With its high speed and ability to perform at above 95% of the earths atmosphere it was designed for defense against a Mach-2 bomber. \nIt had a tilting 2 position wing providing for carrier use. \n\nFichier AIR\nBenoit M. Dubé\ndube_benoit_m@yahoo.fr\n\nversion br3\n2002 mai 06

[EFFECTS]
dirt=fx_tchdrt
[SMOKESYSTEM]
smoke.0=-1.00, -20.00, 0.00, fx_smoke_crusader

[General]
performance=Wing span 39' 11.4" \nLength 58' 8.8"\nHt.16' 4 1\/2"  \nPower Pratt & Whitney J57 with 16,200 lbs thrust.   \nMax. speed with afterburner 1,000 mph.   \n Service Ceiling 40,000. \n Fuel capacity 1,165 gal.   \nArmament four 20 mm cannon and thirty two 2.75" missiles \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=16830.000000
empty_weight_roll_MOI=150000.000000
empty_weight_pitch_MOI=200000.000000
empty_weight_yaw_MOI=350000.000000
empty_weight_coupled_MOI=0.000000
[fuel]
LeftMain=0.000000,0.000000,0.000000,582.000000,0.000000
RightMain=0.000000,0.000000,0.000000,582.000000,0.000000
fuel_type=2.000000
number_of_tank_selectors=1
[airplane_geometry]
wing_area=590.000000
wing_span=37.500000
wing_root_chord=17.250000
wing_dihedral=-1.994019
wing_incidence=-0.488892
wing_twist=-0.994263
oswald_efficiency_factor=1.366258
wing_winglets_flag=0
wing_sweep=0.000000
wing_pos_apex_lon=0.019170
wing_pos_apex_vert=0.000000
htail_area=200.000000
htail_span=25.000000
htail_pos_lon=-21.666667
htail_pos_vert=0.000000
htail_incidence=0.000000
htail_sweep=0.000000
vtail_area=200.000000
vtail_span=16.124515
vtail_sweep=0.000000
vtail_pos_lon=-29.166667
vtail_pos_vert=5.833333
elevator_area=25.000000
aileron_area=23.800000
rudder_area=17.000000
elevator_up_limit=27.501974
elevator_down_limit=27.501974
aileron_up_limit=31.512679
aileron_down_limit=14.896903
rudder_limit=30.000070
elevator_trim_limit=25.783101
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
[contact_points]
point.0=1.000000,9.083333,0.000000,-5.833333,2776.282603,0.000000,0.670737,36.540000,0.206385,2.500000,0.780326,5.000000,5.000000,0.000000,0.000000,0.000000
point.1=1.000000,-3.083333,-10.416667,-5.416667,2776.282603,1.000000,0.670737,0.000000,0.206404,2.500000,0.780284,5.000000,5.000000,2.000000,0.000000,0.000000
point.2=1.000000,-3.083333,10.416667,-5.416667,2776.282603,2.000000,0.670737,0.000000,0.206404,2.500000,0.780284,5.000000,5.000000,3.000000,0.000000,0.000000
point.3=2.000000,-9.333333,-15.666667,0.833333,2776.282603,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,5.000000,0.000000,0.000000
point.4=2.000000,-9.333333,15.666667,0.833333,2776.282603,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,6.000000,0.000000,0.000000
point.5=2.000000,-19.583333,0.000000,-1.500000,2776.282603,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,9.000000,0.000000,0.000000
point.6=2.000000,9.083333,0.000000,-1.500000,2776.282603,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,4.000000,0.000000,0.000000
static_pitch=2.059937
static_cg_height=5.256553
[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=9.998114,0.000000
flaps-position.2=19.996227,0.000000
flaps-position.3=29.994341,0.000000
flaps-position.4=39.992454,0.000000
[GeneralEngineData]
engine_type=1
Engine.0=0.000000,0.000000,0.000000
fuel_flow_scalar=1.000000
[TurbineEngineData]
fuel_flow_gain=0.025000
inlet_area=0.500000
rated_N2_rpm=29920.000000
static_thrust=13500.000000
afterburner_available=1
reverser_available=1
[Reference Speeds]
flaps_up_stall_speed=100.000000
full_flaps_stall_speed=80.000000
cruise_speed=460.724396
[keyboard_response]
elevator=150.000000,250.000000
aileron=150.000000,250.000000
rudder=150.000000,250.000000
[Views]
eyepoint=11.252256,0.000000,2.076156
[autopilot]
autopilot_available=1
flight_director_available=1
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