[fltsim.0] title=F-2A JASDF sim=F-2A JASDF model= panel= sound= texture= checklists= ui_manufacturer=Mitsubishi ui_type=F-2A ui_variation=No.515 for Actual combat disposition(Misawa base) description="Excerpt from homepage of Mitsubishi Heavy Industires"\n\nF-2 concentrates the technology with excellent Japan-U.S. to suit an operation plan of our country and a geographic characteristic, etc. , and is development of fighter F-16C of the United States by the Japan-U.S. cooperation to deal doing of support fighter (F-1). \n\n Feature of F-2\nF-2 installs an active, phased-array radar to improve standoff vs. warship attack power, and enables installing long distance ASM. \nMoreover, the adoption of the large thrust engine is lightened to obtain a high air defense combat ability accelerated etc. high turn/and, and, the airframe structure is lightened. \nIn addition, FBW (care free, electronic control system) from which reinforced windshield and integration and electron war system are adopted to improve survivability, and it is prevented automatically by dangerous flight condition. \nby Kazunori Ito [fltsim.1] title=XF-2 sim=F-2A JASDF model=XF2 panel= sound= texture=XF2 checklists= ui_manufacturer=Mitsubishi ui_type=F-2A ui_variation=Prototype XF-2 first airplaneiMisawa basej description="Excerpt from homepage of Mitsubishi Heavy Industires"\n\nF-2 concentrates the technology with excellent Japan-U.S. to suit an operation plan of our country and a geographic characteristic, etc. , and is development of fighter F-16C of the United States by the Japan-U.S. cooperation to deal doing of support fighter (F-1). \n\n Feature of F-2\nF-2 installs an active, phased-array radar to improve standoff vs. warship attack power, and enables installing long distance ASM. \nMoreover, the adoption of the large thrust engine is lightened to obtain a high air defense combat ability accelerated etc. high turn/and, and, the airframe structure is lightened. \nIn addition, FBW (care free, electronic control system) from which reinforced windshield and integration and electron war system are adopted to improve survivability, and it is prevented automatically by dangerous flight condition. \nby Kazunori Ito [General] performance=Crew - one person\nEngine - F110-GE/IHI-129 \nTotal length - 15.52m\nWidth - 11.13m\nTotal height - 4.96m\nMaximum speed - about Mach 2.0\nCruising range - about 4,000km\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,-7.500000,2952.755906,0.000000,0.842960,36.360000,1.221440,2.500000,0.573540,5.000000,5.000000,0.000000,0.000000,0.000000 point.1=1.000000,-6.333333,-4.250000,-6.500000,2952.755906,1.000000,0.842960,0.000000,0.323441,2.500000,0.582204,5.000000,5.000000,2.000000,0.000000,0.000000 point.2=1.000000,-6.333333,4.250000,-6.500000,2952.755906,2.000000,0.842960,0.000000,0.323441,2.500000,0.582204,5.000000,5.000000,3.000000,0.000000,0.000000 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=-16.666667,0.000000,0.000000 fuel_flow_scalar=1.000000 [TurbineEngineData] fuel_flow_gain=0.000904 inlet_area=67.404000 rated_N2_rpm=29920.000000 static_thrust=56170.000000 afterburner_available=0 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
