[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