[fltsim.0] title=jstar2 sim=jstar2 model= panel= sound= texture= checklists= atc_id=N771J ui_manufacturer=Lockheed Martin ui_type=Jetstar II ui_variation=White with Red description=First flown in 1957, the JetStar was upgraded to the JetStar II in 1975. This one was made with FSDS by ABACUS. atc_heavy=0 atc_airline= atc_flight_number= [General] atc_type=Jetstar atc_model=II editable=1 performance=Cruise Speed: 500 kts\nRange: 2,770 nm\nCeiling: 45,000 ft\nSeating: 10\nDesigner: Chuck Dome\nDate: March, 2002 [Radios] // Radio Type=availiable, standby frequency, has glide slope Audio.1=1 Com.1=1, 1 Com.2=1, 1 Nav.1=1, 1, 1 Nav.2=1, 1, 0 Adf.1=1 Transponder.1=1 Marker.1=1 [forcefeedback] stick_shaker_magnitude=5000 ; 0 - 10000 stick_shaker_direction=0 ; 0 - 35999 degrees stick_shaker_period=111111 ; in microseconds gear_bump_nose_magnitude=3000 ; 0 - 10000 gear_bump_nose_direction=18000 ; 0 - 35999 degrees gear_bump_nose_duration=250000 ; in microseconds gear_bump_left_magnitude=2700 ; 0 - 10000 gear_bump_left_direction=9000 ; 0 - 35999 degrees gear_bump_left_duration=250000 ; in microseconds gear_bump_right_magnitude=2700 ; 0 - 10000 gear_bump_right_direction=27000 ; 0 - 35999 degrees gear_bump_right_duration=250000 ; in microseconds ground_bumps_magnitude1=1300 ; 0 - 10000 ground_bumps_angle1=08900 ; 0 - 35999 degrees ground_bumps_intercept1=3.0 ground_bumps_slope1=0.20 ground_bumps_magnitude2=200 ; 0 - 10000 ground_bumps_angle2=09100 ; 0 - 35999 degrees ground_bumps_intercept2=1.075 ground_bumps_slope2=0.035 crash_magnitude1=10000 ; 0 - 10000 crash_direction1=01000 ; 0 - 35999 degrees crash_magnitude2=10000 ; 0 - 10000 crash_direction2=9000 ; 0 - 35999 degrees crash_period2=75000 ; in microseconds crash_duration2=2500000 ; in microseconds [WEIGHT_AND_BALANCE] reference_datum_position= 0.000, 0.000, 0.000 empty_weight_CG_position= 0.000, 0.000, 0.000 max_number_of_stations=50 station_load.0=0.000000,0.000000,0.000000,0.000000 empty_weight= 8000.000 empty_weight_roll_MOI= 47500.000 empty_weight_pitch_MOI= 92500.000 empty_weight_yaw_MOI= 77500.000 empty_weight_coupled_MOI= 3300.000 max_gross_weight= 13360.000 CG_forward_limit= 0.000 CG_aft_limit= 1.000 [fuel] LeftMain= -0.500, -6.000, 0.000, 400.000, 0.000 RightMain= -0.500, 6.000, 0.000, 400.000, 0.000 fuel_type=2.000000 number_of_tank_selectors=1 [airplane_geometry] wing_area= 275.000 wing_span= 44.000 wing_root_chord= 6.250 wing_dihedral= 2.499 wing_incidence= 0.000 wing_twist= -1.500 oswald_efficiency_factor= 0.857 wing_winglets_flag= 0 wing_sweep= 0.000 wing_pos_apex_lon= 0.019 wing_pos_apex_vert= 0.000 htail_area= 57.000 htail_span= 17.500 htail_pos_lon= -24.583 htail_pos_vert= 0.000 htail_incidence= 1.000 htail_sweep= 0.000 vtail_area= 64.000 vtail_span= 9.121 vtail_sweep= 0.000 vtail_pos_lon= -20.500 vtail_pos_vert= 6.833 elevator_area= 16.700 aileron_area= 14.500 rudder_area= 10.700 elevator_up_limit= 24.500 elevator_down_limit= 21.000 aileron_up_limit= 26.500 aileron_down_limit= 21.500 rudder_limit= 25.000 elevator_trim_limit= 18.500 spoiler_limit= 60.000 spoilerons_available= 1 aileron_to_spoileron_gain= 4.600 min_ailerons_for_spoilerons= 4.985 min_flaps_for_spoilerons= 0.000 [contact_points] point.0= 1.000, 15.750, 0.000, -3.200, 1180.454, 0.000, 0.593, 41.340, 0.180, 2.500, 0.825, 5.000, 5.000, 0.000, 0.000, 0.000 point.1= 1.000, -2.083, -5.417, -3.300, 1573.938, 1.000, 0.593, 0.000, 0.323, 2.500, 0.832, 5.000, 5.000, 2.000, 0.000, 0.000 point.2= 1.000, -2.083, 5.417, -3.300, 1573.938, 2.000, 0.593, 0.000, 0.323, 2.500, 0.832, 5.000, 5.000, 3.000, 0.000, 0.000 point.3= 2.000, -3.333, -23.917, 0.000, 787.402, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 5.000, 0.000, 0.000 point.4= 2.000, -3.333, 23.917, 0.000, 787.402, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 6.000, 0.000, 0.000 point.5= 2.000, -22.667, 0.000, 0.000, 1180.454, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 9.000, 0.000, 0.000 point.6= 2.000, 23.083, 0.000, 0.000, 1180.454, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 4.000, 0.000, 0.000 static_pitch= 0.000 static_cg_height= 2.753 [GeneralEngineData] engine_type= 1 Engine.0= -6.500, -8.000, 0.833 Engine.1= -6.500, -5.000, 0.833 Engine.2= -6.500, 5.000, 0.833 Engine.3= -6.500, 8.000, 0.833 fuel_flow_scalar= 0.500 [TurbineEngineData] fuel_flow_gain= 0.100 inlet_area= 3.000 rated_N2_rpm= 29920.000 static_thrust= 1600.000 afterburner_available= 0 reverser_available= 1 [Reference Speeds] flaps_up_stall_speed= 100.000 full_flaps_stall_speed= 80.000 cruise_speed= 624.682 [keyboard_response] elevator=150.000000,250.000000 aileron=150.000000,250.000000 rudder=150.000000,250.000000 [Views] eyepoint=20.210486,-1.589157,5.626128 [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 use_no_default_bank=1 [direction_indicators] direction_indicator.0=3,0 [Flaps.0] type= 1 span-outboard= 0.500 extending-time= 5.000 system_type= 0 damaging-speed= 0.000 blowout-speed= 0.000 lift_scalar= 1.000 drag_scalar= 1.000 pitch_scalar= 1.000 flaps-position.0= 0.000, 0.000 flaps-position.1= 10.000, 0.000 flaps-position.2= 20.000, 0.000 flaps-position.3= 30.000, 0.000 [jet_engine] thrust_scalar=1.000 [flight_tuning] cruise_lift_scalar=1.000 pitch_stability=1.000 roll_stability=1.000 yaw_stability=1.000 parasite_drag_scalar=1.000 induced_drag_scalar=1.000 elevator_effectiveness=1.000 aileron_effectiveness=1.000 rudder_effectiveness=1.000 elevator_trim_effectiveness=1.000 aileron_trim_effectiveness=1.000 rudder_trim_effectiveness=1.000
