[fltsim.0]
title=HO-229A Day Fighter 1
sim=HO-229
model=A
panel=
sound=
texture=A23
kb_checklists=
//ui_manufacturer=ŽÀŒ±‹@/ŽŽì‹@
//ui_type=Horten HO-229
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

[fltsim.1]
title=HO-229A Day Fighter 2
sim=HO-229
model=A
panel=
sound=
texture=A00
kb_checklists=
//ui_manufacturer=ŽÀŒ±‹@/ŽŽì‹@
//ui_type=Horten HO-229
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

[fltsim.2]
title=HO-229A Day Fighter 3
sim=HO-229
model=A
panel=
sound=
texture=A35
kb_checklists=
//ui_manufacturer=ŽÀŒ±‹@/ŽŽì‹@
//ui_type=Horten HO-229
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

[fltsim.3]
title=HO-229B
sim=HO-229
model=B
panel=
sound=
texture=B21
kb_checklists=
//ui_manufacturer=ŽÀŒ±‹@/ŽŽì‹@
//ui_type=Horten HO-229
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

[fltsim.4]
title=HO-229B Night Fighter 1
sim=HO-229
model=BN
panel=
sound=
texture=B10
kb_checklists=
//ui_manufacturer=ŽÀŒ±‹@/ŽŽì‹@
//ui_type=Horten HO-229
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

[fltsim.5]
title=HO-229B Night Fighter 2
sim=HO-229
model=BN
panel=
sound=
texture=B01
kb_checklists=
//ui_manufacturer=ŽÀŒ±‹@/ŽŽì‹@
//ui_type=Horten HO-229
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

[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

[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=7600.000000
empty_weight_roll_MOI=28000.000000
empty_weight_pitch_MOI=48000.000000
empty_weight_yaw_MOI=24000.000000
empty_weight_coupled_MOI=1300.000000

[fuel]
Center1=0.000000,0.000000,0.000000,68.000000,0.000000
LeftMain=0.000000,0.000000,0.000000,74.000000,0.000000
LeftAux=0.000000,-5.000000,0.000000,35.000000,0.000000
LeftTip=0.000000,-10.000000,0.000000,26.000000,0.000000
RightMain=0.000000,0.000000,0.000000,74.000000,0.000000
RightAux=0.000000,5.000000,0.000000,35.000000,0.000000
RightTip=0.000000,10.000000,0.000000,26.000000,0.000000
fuel_type=2.000000
number_of_tank_selectors=1

[airplane_geometry]
wing_area=200.000000
wing_span=30.500000
wing_root_chord=7.333333
wing_dihedral=0.000000
wing_incidence=-0.494385
wing_twist=0.000000
oswald_efficiency_factor=1.871080
wing_winglets_flag=0
wing_sweep=0.000000
wing_pos_apex_lon=0.000000
wing_pos_apex_vert=0.000000
htail_area=47.000000
htail_span=14.166667
htail_pos_lon=-16.333333
htail_pos_vert=0.000000
htail_incidence=0.000000
htail_sweep=0.000000
vtail_area=40.000000
vtail_span=7.211103
vtail_sweep=0.000000
vtail_pos_lon=-16.333333
vtail_pos_vert=5.833333
elevator_area=7.500000
aileron_area=6.880000
rudder_area=3.400000
elevator_up_limit=28.647890
elevator_down_limit=28.647890
aileron_up_limit=17.761692
aileron_down_limit=17.761692
rudder_limit=22.918312
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= 1.000, 9.917, 0.000, -7.900, 1574.803, 0.000, 0.632, 37.140, 0.990, 2.500, 0.407, 5.000, 5.000, 0.000, 0.000, 0.000
point.1= 1.000, -2.833, -3.917, -5.100, 1574.803, 1.000, 0.632, 0.000, 0.404, 2.500, 0.595, 5.000, 5.000, 2.000, 0.000, 0.000
point.2= 1.000, -2.833, 3.917, -5.100, 1574.803, 2.000, 0.632, 0.000, 0.404, 2.500, 0.595, 5.000, 5.000, 3.000, 0.000, 0.000
point.3= 2.000, -8.000, -13.833, -1.333, 1574.803, 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, -8.000, 13.833, -1.333, 1574.803, 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, -18.667, 0.000, -1.000, 1574.803, 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, 18.583, 0.000, -0.500, 1574.803, 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= 6.000

[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=19.999092,0.000000
flaps-position.2=39.998184,0.000000

[GeneralEngineData]
engine_type=1
Engine.0= 0.000, -1.180, 0.417
Engine.1= 0.000, 1.180, 0.417
fuel_flow_scalar=1.000000

[TurbineEngineData]
fuel_flow_gain=0.002170
inlet_area=4.471680
rated_N2_rpm=29920.000000
static_thrust=2693.000000
afterburner_available=0
reverser_available=1

[Reference Speeds]
flaps_up_stall_speed=82.000000
full_flaps_stall_speed=65.600000
cruise_speed=456.372410

[keyboard_response]
elevator=150.000000,250.000000
aileron=150.000000,250.000000
rudder=150.000000,250.000000

[autopilot]
autopilot_available=1
flight_director_available=0
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

[direction_indicators]
direction_indicator.0=3,0

[Views]
eyepoint=9.356666,0.000000,1.300000

[EFFECTS]
wake=fx_wake
water=fx_spray
dirt=fx_tchdrt
concrete=fx_sparks
touchdown=fx_tchdwn, 1

[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,  -6.33, 27.17, 1.02, fx_navgre ,
light.1=3,  -6.33, -27.17, 1.02, fx_navred ,

light.2=3,  -11.71, 0.00, -0.46, fx_navwhi ,