[fltsim.0] title=HO-229A Day Fighter 1 sim=HO_229 model=A panel= sound= texture=A23 kb_checklists=Ho-229_check ui_manufacturer=Horten ui_type=HO-229 ui_variation=Type A (Paint1) description=This was a flying-wing fighter-bomber project whose first rototype made its maiden flight in 1945.\nIt is expected performance and armament were great and it was the first flying-wing with turbojets. \nThere was a B version planned which was intended as night fighter with radar and 2 crew member. \nOne of the main drawbacks of this design was that it was limited in the choice of engines; for example, the sronger HeS 011 turbojet, which was in development, would have had a too big diameter for fitting it into the engine slots of this flying-wing. \nThis was one of the main reasons why the Gotha engineers which recieved the Ho IX plans for production preparations designed the Gotha project Go P.60 with each one tubojet over and under the centerline.\n\nby Kazunori Ito\n Kazu16643VT@aol.com\n atc_id=HO229 [fltsim.1] title=HO-229A Day Fighter 2 sim=HO_229 model=A panel= sound= texture=A00 kb_checklists=Ho-229_check ui_manufacturer=Horten ui_type=HO-229 ui_variation=Type A (Paint2) description=This was a flying-wing fighter-bomber project whose first rototype made its maiden flight in 1945.\nIt is expected performance and armament were great and it was the first flying-wing with turbojets. \nThere was a B version planned which was intended as night fighter with radar and 2 crew member. \nOne of the main drawbacks of this design was that it was limited in the choice of engines; for example, the sronger HeS 011 turbojet, which was in development, would have had a too big diameter for fitting it into the engine slots of this flying-wing. \nThis was one of the main reasons why the Gotha engineers which recieved the Ho IX plans for production preparations designed the Gotha project Go P.60 with each one tubojet over and under the centerline.\n\nby Kazunori Ito\n Kazu16643VT@aol.com\n atc_id=HO229 [fltsim.2] title=HO-229A Day Fighter 3 sim=HO_229 model=A panel= sound= texture=A35 kb_checklists=Ho-229_check ui_manufacturer=Horten ui_type=HO-229 ui_variation=Type A (Paint3) description=This was a flying-wing fighter-bomber project whose first rototype made its maiden flight in 1945.\nIt is expected performance and armament were great and it was the first flying-wing with turbojets. \nThere was a B version planned which was intended as night fighter with radar and 2 crew member. \nOne of the main drawbacks of this design was that it was limited in the choice of engines; for example, the sronger HeS 011 turbojet, which was in development, would have had a too big diameter for fitting it into the engine slots of this flying-wing. \nThis was one of the main reasons why the Gotha engineers which recieved the Ho IX plans for production preparations designed the Gotha project Go P.60 with each one tubojet over and under the centerline.\n\nby Kazunori Ito\n Kazu16643VT@aol.com\n atc_id=HO229 [fltsim.3] title=HO-229B sim=HO_229 model=B panel= sound= texture=B21 kb_checklists=Ho-229_check ui_manufacturer=Horten ui_type=HO-229 ui_variation=Type B description=This was a flying-wing fighter-bomber project whose first rototype made its maiden flight in 1945.\nIt is expected performance and armament were great and it was the first flying-wing with turbojets. \nThere was a B version planned which was intended as night fighter with radar and 2 crew member. \nOne of the main drawbacks of this design was that it was limited in the choice of engines; for example, the sronger HeS 011 turbojet, which was in development, would have had a too big diameter for fitting it into the engine slots of this flying-wing. \nThis was one of the main reasons why the Gotha engineers which recieved the Ho IX plans for production preparations designed the Gotha project Go P.60 with each one tubojet over and under the centerline.\n\nby Kazunori Ito\n Kazu16643VT@aol.com\n atc_id=HO229 [fltsim.4] title=HO-229B Night Fighter 1 sim=HO_229 model=BN panel= sound= texture=B10 kb_checklists=Ho-229_check ui_manufacturer=Horten ui_type=HO-229 ui_variation=Type B (Night Fighter) Paint1 description=This was a flying-wing fighter-bomber project whose first rototype made its maiden flight in 1945.\nIt is expected performance and armament were great and it was the first flying-wing with turbojets. \nThere was a B version planned which was intended as night fighter with radar and 2 crew member. \nOne of the main drawbacks of this design was that it was limited in the choice of engines; for example, the sronger HeS 011 turbojet, which was in development, would have had a too big diameter for fitting it into the engine slots of this flying-wing. \nThis was one of the main reasons why the Gotha engineers which recieved the Ho IX plans for production preparations designed the Gotha project Go P.60 with each one tubojet over and under the centerline.\n\nby Kazunori Ito\n Kazu16643VT@aol.com\n atc_id=HO229 [fltsim.5] title=HO-229B Night Fighter 2 sim=HO_229 model=BN panel= sound= texture=B01 kb_checklists=Ho-229_check ui_manufacturer=Horten ui_type=HO-229 ui_variation=Type B (Night Fighter) Paint2 description=This was a flying-wing fighter-bomber project whose first rototype made its maiden flight in 1945.\nIt is expected performance and armament were great and it was the first flying-wing with turbojets. \nThere was a B version planned which was intended as night fighter with radar and 2 crew member. \nOne of the main drawbacks of this design was that it was limited in the choice of engines; for example, the sronger HeS 011 turbojet, which was in development, would have had a too big diameter for fitting it into the engine slots of this flying-wing. \nThis was one of the main reasons why the Gotha engineers which recieved the Ho IX plans for production preparations designed the Gotha project Go P.60 with each one tubojet over and under the centerline.\n\nby Kazunori Ito\n Kazu16643VT@aol.com\n atc_id=HO229 [General] performance=Engines:\n Two Junkers Jumo 004B turbojets\n Thrust: 1,980lb (900kg)\n\nDimensions:\n Span 16.75m\n Length 7.47m\n Height 2.80m\n\nWeights:\n Empty: 10,140lbs (4600kg)\n Max. loaded: 19,840lb (9000kg)\n\nSpeed:\n 607mph (977km/h)\nCeiling:\n 52,500ft (16,000m)\n\nRange:\n 1,970 miles (3170km) at 393mph (635km/h) with two drop tanks\n\nArmaments: Planned\n Four Mk 103 or Mk 108 cannon\n Plus\n Two 1,000kg bombs\n Category=airplane editable=0 atc_type=EXPERIMENTAL atc_model= [weight_and_balance] // ACM V2.3 max_gross_weight = 20725 empty_weight = 10660 reference_datum_position = 0, 0, 0 empty_weight_CG_position = 0, 0, 0 empty_weight_pitch_MOI = 96841 empty_weight_roll_MOI = 64718 empty_weight_yaw_MOI = 104154 empty_weight_coupled_MOI = 0 max_number_of_stations = 1 station_load.0 = 170.00,-3.4,0.0,0.0 [GeneralEngineData] //0=Piston, 1=Jet, 2=None, 3=Helo-Turbine, 4=Rocket, 5=Turboprop engine_type = 1 fuel_flow_scalar = 1 engine.0 = -6,-2.7,0 engine.1 = -6,2.7,0 min_throttle_limit=0.000000 [fuel] //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons) fuel_type = 2 number_of_tank_selectors = 1 Center1 = 0, 0, 0, 0, 0 LeftMain = 0, -5, 0, 200, 0 LeftAux = 0, -2, 0, 135, 0 //RightMain = 0, 2, 0, 200, 0 RightMain = 0, 5, 0, 200, 0 //RightAux = 0, 5, 0, 135, 0 RightAux = 0, 2, 0, 135, 0 electric_pump=0 [contact_points] static_pitch = 12 //static_pitch = 0 //static_cg_height = 7.42 static_cg_height = 5.3 max_number_of_points = 10 //point.0 = 1, 3, 0, -8.1, 1850, 0, 1.8, 25, 0.4197, 2.5, 0.75, 22, 18, 0, 220, 270 point.0 = 1, 3, 0, -6.4, 1850, 0, 1.8, 25, 0.4197, 2.5, 0.75, 22, 18, 0, 220, 270 //point.1 = 1, -8.5, -5.9, -6.5, 2000, 1, 1.2, 0, 0.4798, 2.5, 0.85, 12, 8, 2, 220, 270 point.1 = 1, -8.5, -5.8, -3.99, 2000, 1, 1.2, 0, 0.4798, 2.5, 0.85, 12, 8, 2, 220, 270 //point.2 = 1, -8.5, 5.9, -6.4, 2000, 2, 1.2, 0, 0.4798, 2.5, 0.85, 14, 10, 3, 220, 270 point.2 = 1, -8.5, 5.8, -3.99, 2000, 2, 1.2, 0, 0.4798, 2.5, 0.85, 14, 10, 3, 220, 270 point.3 = 2.0,0,0,0,2100,0,0,0,0,0,0,0,0,4.0,0,0 point.4 = 2.0,-9.0,0,-1.8,2000.4,0,0,0,0,0,0,0,0,4.0,0,0 point.5 = 2.0,-20.4,-27.4,1.3,787.4,0,0,0,0,0,0,0,0,5.0,0,0 point.6 = 2.0,-20.4,27.4,1.3,787.4,0,0,0,0,0,0,0,0,6.0,0,0 point.7 = 2, -18, 0, -1.6, 1500.4, 0, 0, 0, 0, 0, 0, 0, 0, 9, 0, 0 point.8 = 2, -7.7, -14, 1.3, 1000, 0, 0, 0, 0, 0, 0, 0, 0, 5, 0, 0 point.9 = 2, -7.7, 14, 1.3, 1000, 0, 0, 0, 0, 0, 0, 0, 0, 6, 0, 0 gear_system_type=1 [keyboard_response] elevator = 150, 250 aileron = 150, 250 rudder = 150, 250 [forcefeedback] gear_bump_nose_magnitude = 3000 gear_bump_nose_direction = 18000 gear_bump_nose_duration = 250000 gear_bump_left_magnitude = 2700 gear_bump_left_direction = 27000 gear_bump_left_duration = 250000 gear_bump_right_magnitude = 2700 gear_bump_right_direction = 27000 gear_bump_right_duration = 250000 ground_bumps_magnitude1 = 1300 ground_bumps_angle1 = 08900 ground_bumps_intercept1 = 3.0 ground_bumps_slope1 = 0.20 ground_bumps_magnitude2 = 200 ground_bumps_angle2 = 09100 ground_bumps_intercept2 = 1.075 ground_bumps_slope2 = 0.035 crash_magnitude1 = 10000 crash_direction1 = 01000 crash_magnitude2 = 10000 crash_direction2 = 9000 crash_period2 = 75000 crash_duration2 = 2500000 stick_shaker_magnitude = 5000 stick_shaker_direction = 0 stick_shaker_period = 111111 [airplane_geometry] //ACM_AREAW1// 0,0,0,4.4774,0.9312,0.9312,0.6521,4.9057,1.8625,1.8625 //ACM_AREAW2// 1.3042,5.3340,2.7939,2.7939,1.9563,5.7621,3.7253,3.7253,2.6085,6.1904 //ACM_AREAW3// 4.6565,4.6565,3.2606,6.6187,5.5879,5.5879,3.9126,7.0469,6.5192,6.5192 //ACM_AREAW4// 4.5647,7.4752,7.4506,7.4506,5.2170,7.9035,8.3818,8.3818,5.8691,8.3317 //ACM_AREAH1// 0,0,0,1.2942,0.2157,0.2157,0.1509,1.3806,0.4314,0.4314 //ACM_AREAH2// 0.3021,1.4670,0.6470,0.6470,0.4530,1.5534,0.8629,0.8629,0.6042,1.6397 //ACM_AREAH3// 1.0786,1.0786,0.7552,1.7259,1.2942,1.2942,0.9063,1.8123,1.5101,1.5101 //ACM_AREAH4// 1.0572,1.8986,1.7258,1.7258,1.2084,1.9850,1.9414,1.9414,1.3595,2.0713 //ACM_AREAV1// 0,0,0,1.7883,0.1986,0.1986,0.1667,1.8119,0.3973,0.3973 //ACM_AREAV2// 0.3334,1.8356,0.5960,0.5960,0.5001,1.8593,0.7947,0.7947,0.6668,1.8828 //ACM_AREAV3// 0.9934,0.9934,0.8335,1.9065,1.1921,1.1921,1.0003,1.9301,1.3909,1.3909 //ACM_AREAV4// 1.1670,1.9538,1.5895,1.5895,1.3337,1.9775,1.7883,1.7883,1.5004,2.0011 //ACM_CAREAW1// 4.1908,4.1908,5.1732,6.0687,4.6565,4.6565,5.4993,6.3501,5.1223,5.1223 //ACM_CAREAW2// 5.8253,6.6314,5.5879,5.5879,6.1515,6.9126,6.0535,6.0535,6.4774,7.1939 //ACM_CAREAW3// 6.5192,6.5192,6.8035,7.4752,6.9850,6.9850,7.1297,7.7564,7.4506,7.4506 //ACM_CAREAW4// 7.4556,8.0377,7.9162,7.9162,7.7817,8.3191,8.3818,8.3818,8.1077,8.6003 //ACM_CAREAH1// 0,0,0.6470,1.2942,0.2157,0.2157,0.7982,1.4129,0.4314,0.4314 //ACM_CAREAH2// 0.9492,1.5317,0.6470,0.6470,1.1002,1.6504,0.8629,0.8629,1.2513,1.7690 //ACM_CAREAH3// 1.0786,1.0786,1.4024,1.8877,1.2942,1.2942,1.5535,2.0065,1.5101,1.5101 //ACM_CAREAH4// 1.7044,2.1252,1.7258,1.7258,1.8555,2.2439,1.9414,1.9414,2.0067,2.3626 //ACM_CAREAV1// 0,0,0.4469,1.3411,0.1986,0.1986,0.6137,1.4364,0.3973,0.3973 //ACM_CAREAV2// 0.7804,1.5315,0.5960,0.5960,0.9472,1.6267,0.7947,0.7947,1.1138,1.7220 //ACM_CAREAV3// 0.9934,0.9934,1.2806,1.8171,1.1921,1.1921,1.4473,1.9124,1.3909,1.3909 //ACM_CAREAV4// 1.6140,2.0076,1.5895,1.5895,1.7809,2.1027,1.7883,1.7883,1.9476,2.1979 wing_area = 568 wing_span = 55 wing_root_chord = 14.68 wing_dihedral = 0 wing_incidence = 0 wing_twist = -1.8 oswald_efficiency_factor = 0.91258 wing_winglets_flag = 0 wing_sweep = 32.5 wing_pos_apex_lon = 10.70 wing_pos_apex_vert = 0 //htail_area = 41 htail_area = 0.0 //htail_span = 12.73 htail_span = 0 htail_pos_lon = -15 htail_pos_vert = 0 htail_incidence = 0 htail_sweep = 35 vtail_area = 0.0 //vtail_span = 5.86 vtail_span = 0 vtail_sweep = 40 vtail_pos_lon = -15 vtail_pos_vert = 0 //elevator_area = 21 //elevator_area = 185 elevator_area = 13 //aileron_area = 62.6 //aileron_area = 140 aileron_area = 43.4 //rudder_area = 11 rudder_area = 0 elevator_up_limit = 28 elevator_down_limit = 25 aileron_up_limit = 20 aileron_down_limit = 15 rudder_limit = 28 elevator_trim_limit = 15 spoiler_limit = 0 aileron_to_spoileron_gain = 0.0 min_ailerons_for_spoilerons = 0.0 min_flaps_for_spoilerons = 0.0 spoilerons_available = 0 auto_spoiler_available=0 positive_g_limit_flaps_up=9.000000 positive_g_limit_flaps_down=8.000000 negative_g_limit_flaps_up=-7.500000 negative_g_limit_flaps_down=-6.500000 [electrical] max_battery_voltage = 24 generator_alternator_voltage = 28 max_generator_alternator_amps = 85 electric_always_available = 0 [Flaps.0] type=1 span-outboard=0.3125 extending-time=9 system_type=0 damaging-speed=220.0 blowout-speed=270.0 lift_scalar=1.0 drag_scalar=1.0 pitch_scalar=1.0 flaps-position.0=0.0 flaps-position.1=7.5 flaps-position.2=15.0 flaps-position.3=22.5 flaps-position.4=30.0 [Reference Speeds] flaps_up_stall_speed=72 full_flaps_stall_speed=64 cruise_speed=478 max_indicated_speed=565 max_mach=1.06 [flight_tuning] cruise_lift_scalar=1.000 parasite_drag_scalar=1.000 induced_drag_scalar=1.000 elevator_effectiveness=1.000 aileron_effectiveness=1.000 rudder_effectiveness=1.000 pitch_stability=1.000 roll_stability=1.000 yaw_stability=1.000 elevator_trim_effectiveness=1.000 aileron_trim_effectiveness=1.000 rudder_trim_effectiveness=1.000 [TurbineEngineData] fuel_flow_gain=0.003 inlet_area=2.8 //rated_N2_rpm=9800.000 rated_N2_rpm=8700.000 static_thrust=1980 //static_thrust=2640 //static_thrust=3960 afterburner_available=0 reverser_available=0 fuel_flow_scalar=4.512 thrust_scalar=1.0 thrustspecificfuelconsumption=1.0 [gear_warning_system] gear_warning_available=1 pct_throttle_limit=0.099976 flap_limit_power=30.022988 flap_limit_idle=15.011494 [brakes] toe_brakes_scale=0.658864 parking_brake=1 [autopilot] autopilot_available=0 flight_director_available=0 [pitot_static] pitot_heat=1.000000 [hydraulic_system] electric_pumps=0 engine_map=1,1,0,0 normal_pressure=152.777778 [vacuum_system] max_pressure=5.150000 vacuum_type=1 electric_backup_pressure=0.000000 engine_map=1,1,0,0 [pneumatic_system] max_pressure=0.000000 bleed_air_scalar=1.000000 [stall_warning] type=1 stick_shaker=0 [attitude_indicators] attitude_indicator.0=1 [turn_indicators] turn_indicator.0=1,0 [deice_system] structural_deice_type=0 [direction_indicators] direction_indicator.0=3,0 [radios] nav.1=1,0,1 [lights] //Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing light.0 = 3, -6.4, -27.2, 1.0, fx_navred light.1 = 3, -12.1, 0.0,-0.3, fx_navwhi light.2 = 3, -6.3, 27.2, 1.0, fx_navgre