[fltsim.0]
title=BV155 V2
sim=BV 155
model=
panel=
sound=
texture=
kb_checklists=
//ui_manufacturer=ŽÀŒ±‹@/ŽŽì‹@
//ui_type=Blohm & Voss BV155 V2
ui_manufacturer=Blohm & Voss
ui_type=BV155 V2
ui_variation=German Air Force
description= The Blohm und Voss Bv 155 was a high-altitude interceptor aircraft intended to be used by the Luftwaffe against raids by USAAF B-29's. \n Work started on the design in 1942, but the design went through a protracted development period for no obvious reason and was still under construction when World War II ended. \n This fighter was designed to be a very high altitude interceptor, and the wings were made incredibly long, and on the wings were large and bulky radiators. \n Performance was poor at low altitudes, but surprisingly good at high altitudes, and the fighter had a ceiling of 56,000 feet. \n\nby Kazunori Ito \n 
\n  Kazu16643VT @aol.com\n

[General]
performance=Wing span: 20.5m (67 ft. 3 in.)\nLength: 12.00m (39ft. 4? in.)\nHeight: 2.98m (9 ft. 9? in.)\nWing Surface Area: N/A\n\nWeights:\nEmpty: 10,734 lb. (4870 kg)\nMaximum: 13,262 lb. (6016 kg)\n\nPower Plant:\nType: DB 603A with TKL 15 turbocharger\nHorsepower: 1,450 hp at 49,210 ft. (15,000m)\n\nMaximum Speed: 429 mph (690km/h)\nInitial climb: N/A\nRange: 895 miles (1440km) at high altitude\nService Ceiling: N/A\n\nArmament:\nHeavy groups of 15, 20 or 30mm cannon proposed\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=8420.000000
empty_weight_roll_MOI=22500.000000
empty_weight_pitch_MOI=100000.000000
empty_weight_yaw_MOI=70000.000000
empty_weight_coupled_MOI=1300.000000

[fuel]
LeftMain=0.000000,0.000000,0.000000,200.000000,0.000000
LeftAux=0.000000,-12.916667,0.000000,100.000000,0.000000
RightMain=0.000000,0.000000,0.000000,200.000000,0.000000
RightAux=0.000000,12.916667,0.000000,100.000000,0.000000
fuel_type=2.000000
number_of_tank_selectors=1

[airplane_geometry]
wing_area=225.000000
wing_span=32.500000
wing_root_chord=6.916667
wing_dihedral=3.999023
wing_incidence=-0.494385
wing_twist=3.999023
oswald_efficiency_factor=1.501761
wing_winglets_flag=0
wing_sweep=0.000000
wing_pos_apex_lon=0.000000
wing_pos_apex_vert=0.000000
htail_area=54.000000
htail_span=14.000000
htail_pos_lon=-21.666667
htail_pos_vert=0.000000
htail_incidence=0.000000
htail_sweep=0.000000
vtail_area=32.000000
vtail_span=6.449806
vtail_sweep=0.000000
vtail_pos_lon=-19.166667
vtail_pos_vert=5.833333
elevator_area=15.000000
aileron_area=11.000000
rudder_area=6.500000
elevator_up_limit=27.501974
elevator_down_limit=20.626481
aileron_up_limit=19.480565
aileron_down_limit=17.188734
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,-25.750000,0.000000,-0.850000,6153.305130,0,0.625997,48.540000,0.305390,2.500000,0.726310,5,5,0,0,0
point.1=1,3.083333,-8.833333,-5.560000,6153.305130,1,0.625997,0.000000,0.407181,2.500000,0.726510,5,5,2,0,0
point.2=1,3.083333,8.833333,-5.560000,6153.305130,2,0.625997,0.000000,0.407181,2.500000,0.726510,5,5,3,0,0
point.3=2,2.083333,-27.083333,2.083333,2475.912819,0,0.000000,0.000000,0.000000,0.000000,0.000000,0,0,5,0,0
point.4=2,2.083333,27.083333,2.083333,2475.912819,0,0.000000,0.000000,0.000000,0.000000,0.000000,0,0,6,0,0
point.5=2,-25.750000,0.000000,-1.333333,2475.912819,0,0.000000,0.000000,0.000000,0.000000,0.000000,0,0,9,0,0
point.6=2,11.250000,0.000000,0.000000,2475.912819,0,0.000000,0.000000,0.000000,0.000000,0.000000,0,0,4,0,0
static_pitch=0.000000
static_cg_height=7.1

[Flaps.0]
type=1
span-outboard=0.500000
extending-time=4.000000
system_type=0
flaps-position.0=0.000000,0.000000
flaps-position.1=13.330818,0.000000
flaps-position.2=26.661636,0.000000
flaps-position.3=39.992454,0.000000

[GeneralEngineData]
engine_type=1
Engine.0=6.00,0.00,0.00
fuel_flow_scalar=1.000000

[TurbineEngineData]
fuel_flow_gain=0.002170
inlet_area=2.285160
rated_N2_rpm=29920.000000
static_thrust=4799.000000
afterburner_available=0
reverser_available=0

[Reference Speeds]
flaps_up_stall_speed=110.000000
full_flaps_stall_speed=88.000000
cruise_speed=260.00000

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

[Views]
eyepoint=4.660000,0.000000,3.120000

[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

[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,  7.64, 32.84,  1.94, fx_navgre ,
light.1=3,  7.64, -32.84,  1.94, fx_navred ,

light.2=3,  -19.65, 0.00, 0.92, fx_navwhi ,