[fltsim.0] title=Jag-marine sim=Jag-GR1 model=fren panel= sound= texture=navy atc_id_enable=1 atc_id=05 atc_flight_number=2 ui_manufacturer=Sepecat ui_type=Jaguar 'Marine' ui_variation=Prototype Marine nationnale kb_checklists=Jaguar_check kb_reference=Jaguar_ref description=prototype Jaguar marine la France réalise un prototype désigné Jaguar M, destiné à son aéronautique navale et modifié pour opérer depuis un porte-avions. Il fait son premier vol le 14 novembre 1969 et effectue plusieurs campagnes d'essais : appontages simulés sur piste à Nîmes, tests sur une catapulte au sol au Royaume-Uni, puis essais en mer à partir du porte-avions Clemenceau. Cette version est cependant abandonnée début 1973 : d'une part le Jaguar s'avérait sous-motorisé, d'autre part il aurait fallu renforcer les catapultes et le pont des porte-avions ce qui générait évidemment un surcoût élevé. atc_id_color=0000000000 visual_damage=0 [General] atc_type=Sepecat performance=Model Designer : Thierry Bourdin [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 [Views] eyepoint=9.3,0,1.5 [weight_and_balance] // ACM V2.2 max_gross_weight = 34612 empty_weight = 16975 reference_datum_position = 0, 0, 0 empty_weight_CG_position = 0, 0, 0 empty_weight_pitch_MOI = 55430 empty_weight_roll_MOI = 7412 empty_weight_yaw_MOI = 35277 empty_weight_coupled_MOI = 0 max_number_of_stations = 0 [lights] //Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing light.0 = 4, 9.89, 0, 0.23, fx_vclight [GeneralEngineData] //0=Piston, 1=Jet, 2=None, 3=Helo-Turbine, 4=Rocket, 5=Turboprop engine_type = 1 fuel_flow_scalar = 1.000 engine.0 = -17.200, -1.600, 0.000 engine.1 = -17.200, 1.600, 0.000 min_throttle_limit=0.000000 [smokesystem] smoke.0 = -12.00, -19.00, -2.00, fx_eng_exhaust_gry smoke.1 = -12.00, -19.00, 2.00, fx_eng_exhaust_gry [effects] wake = fx_wake water = fx_spray dirt = fx_tchdrt concrete = fx_sparks touchdown = fx_tiremark_6 contrail = fx_contrail_l [fuel] //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons) fuel_type = 2 number_of_tank_selectors = 1 Center1 = 0, 0, 0, 600, 3 electric_pump=0 [contact_points] static_pitch = 1.6 static_cg_height = 8.2 max_number_of_points = 7 point.0 = 1, 18, 0, -8.8, 2000, 0, 1, 25, 0.11, 3, 0.8, 6, 4, 0, 260, 300 point.1 = 1, -1, -4.6, -8.5, 2500, 1, 1.2, 0, 0.5, 2.5, 0.85, 5, 7, 2, 260, 300 point.2 = 1, -1, 4.6, -8.5, 2500, 2, 1.2, 0, 0.5, 2.5, 0.85, 7, 5, 3, 260, 300 point.3 = 2, -12.128, -14.158, -0.728, 1500, 0, 0, 0, 0, 0, 0, 0, 0, 5, 0, 0 point.4 = 2, -12.128, 14.306, -0.728, 1500, 0, 0, 0, 0, 0, 0, 0, 0, 6, 0, 0 point.5 = 2, -18.275, 0, -3.298, 1500, 0, 0, 0, 0, 0, 0, 0, 0, 9, 0, 0 point.6 = 2, 23.092, 0, -3.465, 1500, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0 gear_system_type=1 [keyboard_response] elevator = 150.000000, 250.000000 aileron = 150.000000, 150.000000 rudder = 150.000000, 250.000000 [forcefeedback] gear_bump_nose_magnitude = 1000 gear_bump_nose_direction = 18000 gear_bump_nose_duration = 250000 gear_bump_left_magnitude = 2000 gear_bump_left_direction = 35500 gear_bump_left_duration = 250000 gear_bump_right_magnitude = 2000 gear_bump_right_direction = 500 gear_bump_right_duration = 250000 ground_bumps_magnitude1 = 1250 ground_bumps_angle1 = 8900 ground_bumps_intercept1 = 5 ground_bumps_slope1 = 0.48 ground_bumps_magnitude2 = 450 ground_bumps_angle2 = 9100 ground_bumps_intercept2 = 0.075 ground_bumps_slope2 = 1 crash_magnitude1 = 2000 crash_direction1 = 1000 crash_magnitude2 = 2000 crash_direction2 = 9000 crash_period2 = 7500 crash_duration2 = 2500000 stick_shaker_magnitude = 2000 stick_shaker_direction = 0 stick_shaker_period = 111111 [airplane_geometry] //ACM_AREAW1// 0,0,0,3.5813,0.4842,0.4842,0.4675,3.8698,0.9685,0.9685 //ACM_AREAW2// 0.9351,4.1585,1.4528,1.4528,1.4026,4.4471,1.9371,1.9371,1.8707,4.7357 //ACM_AREAW3// 2.4214,2.4214,2.3382,5.0244,2.9056,2.9056,2.8059,5.3130,3.3900,3.3900 //ACM_AREAW4// 3.2736,5.6016,3.8743,3.8743,3.7414,5.8902,4.3586,4.3586,4.2090,6.1788 //ACM_AREAH1// 0,0,0,1.3207,0.2201,0.2201,0.2125,1.4673,0.4402,0.4402 //ACM_AREAH2// 0.4250,1.6138,0.6603,0.6603,0.6377,1.7604,0.8805,0.8805,0.8503,1.9069 //ACM_AREAH3// 1.1006,1.1006,1.0628,2.0534,1.3207,1.3207,1.2754,2.2000,1.5405,1.5405 //ACM_AREAH4// 1.4880,2.3464,1.7610,1.7610,1.7006,2.4930,1.9809,1.9809,1.9132,2.6396 //ACM_AREAV1// 0,0,0,2.3041,0.2560,0.2560,0.2560,2.3759,0.5120,0.5120 //ACM_AREAV2// 0.5120,2.4474,0.7680,0.7680,0.7680,2.5192,1.0240,1.0240,1.0240,2.5910 //ACM_AREAV3// 1.2798,1.2798,1.2798,2.6626,1.5361,1.5361,1.5361,2.7344,1.7920,1.7920 //ACM_AREAV4// 1.7920,2.8059,2.0480,2.0480,2.0480,2.8777,2.3041,2.3041,2.3041,2.9493 //ACM_CAREAW1// 2.1793,2.1793,3.8952,4.6114,2.4214,2.4214,4.1290,4.8095,2.6635,2.6635 //ACM_CAREAW2// 4.3628,5.0075,2.9056,2.9056,4.5967,5.2055,3.1479,3.1479,4.8305,5.4036 //ACM_CAREAW3// 3.3900,3.3900,5.0644,5.6016,3.6322,3.6322,5.2982,5.7996,3.8743,3.8743 //ACM_CAREAW4// 5.5321,5.9976,4.1163,4.1163,5.7659,6.1957,4.3586,4.3586,5.9997,6.3937 //ACM_CAREAH1// 0,0,0.6603,1.3207,0.2201,0.2201,0.8729,1.5003,0.4402,0.4402 //ACM_CAREAH2// 1.0855,1.6799,0.6603,0.6603,1.2977,1.8594,0.8805,0.8805,1.5104,2.0390 //ACM_CAREAH3// 1.1006,1.1006,1.7230,2.2186,1.3207,1.3207,1.9357,2.3980,1.5405,1.5405 //ACM_CAREAH4// 2.1484,2.5776,1.7610,1.7610,2.3610,2.7572,1.9809,1.9809,2.5736,2.9368 //ACM_CAREAV1// 0,0,0.5759,1.7280,0.2560,0.2560,0.8320,1.8918,0.5120,0.5120 //ACM_CAREAV2// 1.0880,2.0559,0.7680,0.7680,1.3437,2.2197,1.0240,1.0240,1.6001,2.3835 //ACM_CAREAV3// 1.2798,1.2798,1.8559,2.5473,1.5361,1.5361,2.1122,2.7111,1.7920,1.7920 //ACM_CAREAV4// 2.3682,2.8752,2.0480,2.0480,2.6243,3.0390,2.3041,2.3041,2.8803,3.2028 wing_area = 260.000 wing_span = 28.60 wing_root_chord = 11.75 wing_dihedral = -4 wing_incidence = 1.500 wing_twist = -1.000 oswald_efficiency_factor = 0.883 wing_winglets_flag = 0 wing_sweep = 44 wing_pos_apex_lon = 8.57 wing_pos_apex_vert = 0 htail_area = 43.650 htail_span = 13 htail_pos_lon = -13.42 htail_pos_vert = 0 htail_incidence = 0.000 htail_sweep = 44 vtail_area = 44.000 vtail_span = 7.54 vtail_sweep = 45 vtail_pos_lon = -12.46 vtail_pos_vert = 0.80 elevator_area = 22.000 aileron_area = 26.000 rudder_area = 21.000 elevator_up_limit = 27.915 elevator_down_limit = 19.939 aileron_up_limit = 19.939 aileron_down_limit = 14.954 rudder_limit = 29.908 elevator_trim_limit = 20.054 spoiler_limit = 59.989 aileron_to_spoileron_gain = 0.000 min_ailerons_for_spoilerons = 0.000 min_flaps_for_spoilerons = 0.000 spoilerons_available = 0 [electrical] max_battery_voltage = 24 generator_alternator_voltage = 28 max_generator_alternator_amps = 150 electric_always_available = 0 [direction_indicators] direction_indicator.0=3,0 [TurbineEngineData] fuel_flow_gain=0.002 inlet_area=5.000 rated_N2_rpm=29920.000 static_thrust=5520.000 afterburner_available=1 reverser_available=0 [autopilot] autopilot_available=1 flight_director_available=1 default_vertical_speed=2000.000000 autothrottle_available=1 autothrottle_arming_required=0 autothrottle_takeoff_ga=0 autothrottle_max_rpm=90.000000 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 [jet_engine] thrust_scalar=1.000 [Flaps.0] type= 1 span-outboard= 0.500 extending-time= 5.000 system_type= 1 damaging-speed= 325.000 blowout-speed= 365.000 lift_scalar= 1.000 drag_scalar= 1.000 pitch_scalar= 1.000 flaps-position.0= 0.000, 0.000 flaps-position.1= 15.250, 0.000 flaps-position.2= 30.500, 0.000 flaps-position.3= 45.750, 0.000 flaps-position.4= 70.000, 0.000 [Reference Speeds] flaps_up_stall_speed=160.000000 full_flaps_stall_speed=128.000000 cruise_speed=521.151838 max_indicated_speed=918.000000 max_mach=1.600000 [brakes] toe_brakes_scale=0.808741 parking_brake=1 [gear_warning_system] gear_warning_available=1 pct_throttle_limit=0.099976 flap_limit_power=25.496622 flap_limit_idle=5.042029 [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