[fltsim.0] title=CHING-KUO sim=CHING-KUO model= panel= sound= texture= kb_checklists= //ui_manufacturer=RpWFbg@ //ui_type=AIDC F-CK-1A CHING-KUO ui_manufacturer=AIDC ui_type=F-CK-1A CHING-KUO ui_variation= description=The Taiwanese Ching-Kuo Fighter is developed and manufactured by the Aerospace Industrial Development Corporation based in Taichung. \nThe aircraft is also referred to as the Indigenous Defence Fighter (IDF). \nBecause sales of the fighter were refused by a policy of the United States toward China, Taiwan will develop an original new fighter. \nDevelopment has progressed to original related to cooperation with each aerospace corporate company in the United States because there was no restriction for technical assistance. \n\n\nby Kazunori Ito\n Kazu1664VT@aol.com\n [General] performance=Width: 8.53m\nLength: 14.48m\nHeight: 4.65m\nWing area: 26.00 square m\nWeight: 5500kg\nEngine: AlliedSignal/AIDC TFE1042-70(A/B 4300kg) ~ 2\nCapacity of fuel (inside the plane): 2517 liters\nThe maximum speed: M1.7\nThe surface of the sea rate of increase: 15240m/min\nPractical, rising limit: 16775m\nCruising range: 1500km (standard fuel)\nArms:\n M61A1 20mm (511 bullets)\n Tenken type1 AAM~4 + Tenken types2 AAM~2\n AGM-65~2\nCrew: 1\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=35000.000000 empty_weight_roll_MOI=900000.000000 empty_weight_pitch_MOI=1000000.000000 empty_weight_yaw_MOI=950000.000000 empty_weight_coupled_MOI=1200.000000 [fuel] LeftMain=0.000000,0.000000,0.000000,710.000000,0.000000 LeftAux=0.000000,0.000000,0.000000,370.000000,0.000000 RightMain=0.000000,0.000000,0.000000,710.000000,0.000000 RightAux=0.000000,0.000000,0.000000,370.000000,0.000000 fuel_type=2.000000 number_of_tank_selectors=1 [airplane_geometry] wing_area=806.000000 wing_span=48.333333 wing_root_chord=16.666667 wing_dihedral=0.999756 wing_incidence=-0.494385 wing_twist=-1.999512 oswald_efficiency_factor=1.072628 wing_winglets_flag=18 wing_sweep=0.000000 wing_pos_apex_lon=0.000000 wing_pos_apex_vert=0.000000 htail_area=375.000000 htail_span=29.166667 htail_pos_lon=-29.166667 htail_pos_vert=0.000000 htail_incidence=0.000000 htail_sweep=0.000000 vtail_area=485.000000 vtail_span=25.109759 vtail_sweep=0.000000 vtail_pos_lon=-16.666667 vtail_pos_vert=5.833333 elevator_area=75.000000 aileron_area=27.920000 rudder_area=34.000000 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 [contact_points] point.0=1.000000,8.833333,0.000000,-7.320000,2952.755906,0.000000,0.842960,36.360000,1.221440,2.500000,0.573540,5.000000,5.000000,0.000000,0.000000,0.000000 point.1=1.000000,-7.333333,-4.250000,-6.400000,2952.755906,1.000000,0.842960,0.000000,0.323441,2.500000,0.582204,5.000000,5.000000,2.000000,0.000000,0.000000 point.2=1.000000,-7.333333,4.250000,-6.400000,2952.755906,2.000000,0.842960,0.000000,0.323441,2.500000,0.582204,5.000000,5.000000,3.000000,0.000000,0.000000 point.3=2.000000,-6.166667,-21.000000,0.416667,1574.803150,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,5.000000,0.000000,0.000000 point.4=2.000000,-6.166667,21.000000,0.416667,1574.803150,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,6.000000,0.000000,0.000000 point.5=2.000000,-37.000000,0.000000,-1.083333,1574.803150,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,9.000000,0.000000,0.000000 point.6=2.000000,35.416667,0.000000,-1.666667,1574.803150,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,4.000000,0.000000,0.000000 static_pitch=0.000000 static_cg_height=6.987310 [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=-6.666667,-1.416667,-0.833333 Engine.1=-6.666667,1.416667,-0.833333 fuel_flow_scalar=1.000000 [TurbineEngineData] fuel_flow_gain=0.000904 inlet_area=67.404000 rated_N2_rpm=29920.000000 static_thrust=43000.000000 afterburner_available=1 reverser_available=0 [Reference Speeds] flaps_up_stall_speed=119.000000 full_flaps_stall_speed=95.200000 cruise_speed=629.374230 [keyboard_response] elevator=0.000000,0.000000 aileron=0.000000,0.000000 rudder=0.000000,0.000000 [Views] eyepoint=12.854228,0.000000,3.473077 [autopilot] autopilot_available=1 flight_director_available=0 default_vertical_speed=1800.000000 autothrottle_available=1 autothrottle_arming_required=1 autothrottle_takeoff_ga=1 autothrottle_max_rpm=90.000000 pitch_takeoff_ga=8.000000 [direction_indicators] direction_indicator.0=3,0 [LIGHTS] //Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing //6=taxi light, 7=recognition light, 8=wing light, 9=logo light // Z, X, Y light.0=3, -0.01, 0.00, 1.70, fx_navred , light.1=2, -0.01, 0.00, 1.70, fx_strobe , light.2=3, -21.26, 0.00, 8.62, fx_navwhi , light.3=2, -21.26, 0.00, 8.62, fx_strobe , light.4=3, -22.44, 0.00, 0.31, fx_navwhi , light.5=3, -8.68, 14.26, -0.56, fx_navgre , light.6=2, -8.68, 14.26, -0.56, fx_strobe , light.7=3, -8.68, 14.26, -0.87, fx_navgre , light.8=2, -8.68, 14.26, -0.87, fx_strobe , light.9=3, -8.68, -14.26, -0.56, fx_navred , light.10=2, -8.68, -14.26, -0.56, fx_strobe , light.11=3, -8.68, -14.26, -0.87, fx_navred , light.12=2, -8.68, -14.26, -0.87, fx_strobe , //fx_efaburner = normal point + (Y)3.76 light.11=6, -23.30, 1.49, 2.88, fx_efaburner light.12=6, -23.30, -1.49, 2.88, fx_efaburner
