[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