[fltsim.0]
title=He P1079B/II
sim=p1079b
model=
panel=
sound=
texture=
kb_checklists=p1079b_check
kb_reference=p1079b_ref
atc_id=E400HE
atc_airline=
atc_flight_number=
ui_manufacturer=Heinkel
ui_type=He P1079B/II Prototype
ui_variation=Polished Aluminium
visual_damage=1
description=This aircraft is based on  the second design  for the He P.1079B all-weather heavy fighter. The wings were swept back sharply and contained six fuel tanks. Two He S 011 jet engines were located in the wing roots and were fed by intakes in the wing leading edges. A crew of two sat back-to-back in the cockpit, and armament was to be four MK 108 30mm cannon. No evidence has been found that the P.1079 projects were ever submitted to the RLM, but it is known that designer Siegfried Günter, along with his engineers Eichner and Hohbach, were working on these designs under U.S. supervision during the summer of 1945. \nThis is a modern version where the co-pilot faces the front.
atc_heavy=0


[forcefeedback]
gear_bump_nose_magnitude=6000           ; 0 - 10000
gear_bump_nose_direction=18000          ; 0 - 35999 degrees
gear_bump_nose_duration=250000          ; in microseconds
gear_bump_left_magnitude=6000           ; 0 - 10000
gear_bump_left_direction=35500          ; 0 - 35999 degrees
gear_bump_left_duration=250000          ; in microseconds
gear_bump_right_magnitude=6000          ; 0 - 10000
gear_bump_right_direction=00500         ; 0 - 35999 degrees
gear_bump_right_duration=250000         ; in microseconds
ground_bumps_magnitude1=3250            ; 0 - 10000
ground_bumps_angle1=8900                ; 0 - 35999 degrees
ground_bumps_intercept1=5.0
ground_bumps_slope1=0.48
ground_bumps_magnitude2=750             ; 0 - 10000
ground_bumps_angle2=9100                ; 0 - 35999 degrees
ground_bumps_intercept2=0.075
ground_bumps_slope2=1.0
crash_magnitude1=10000                  ; 0 - 10000
crash_direction1=01000                  ; 0 - 35999 degrees
crash_magnitude2=10000                  ; 0 - 10000
crash_direction2=9000                   ; 0 - 35999 degrees
crash_period2=75000                     ; in microseconds
crash_duration2=2500000                 ; in microseconds

[General]
performance=Span: 43ft\nLength: 31ft\nDry weight: 15000 lb\nFuel capacity: 2200 gal\nTakeoff weight: 29735 lb\nMax speed: 834 knots\nMax height: 60000 ft\nMax range: 2100 miles\nCheck the notes for more info.
atc_type=
atc_model=

[WEIGHT_AND_BALANCE]
reference_datum_position=0.000, 0.000, 0.000
empty_weight_CG_position=0.000, 0.000, 0.000
max_number_of_stations=50
station_load.0=0.000000,0.000000,0.000000,0.000000
empty_weight=15000.000000
empty_weight_roll_MOI=135000.000000
empty_weight_pitch_MOI=262662.000000
empty_weight_yaw_MOI=373480.000000
empty_weight_coupled_MOI=1300.000000
max_gross_weight=46388.000

[fuel]
LeftMain=0.000, 0.000, 0.000, 700.000, 0.000
RightMain=0.000, 0.000, 0.000, 700.000, 0.000
Center1=0.000, 0.000, 0.000, 800.000, 0.000
fuel_type=2.000000
number_of_tank_selectors=1

[airplane_geometry]
wing_area=608.000000
wing_span=46.666667
wing_root_chord=13.000000
wing_dihedral=-0.049438
wing_incidence=-0.494385
wing_twist=-0.999756
oswald_efficiency_factor=126.608319
wing_winglets_flag=0
wing_sweep=0.000000
wing_pos_apex_lon=0.000000
wing_pos_apex_vert=0.000000
htail_area=80.000000
htail_span=20.000000
htail_pos_lon=-14.166667
htail_pos_vert=0.000000
htail_incidence=0.000000
htail_sweep=0.000000
vtail_area=140.000000
vtail_span=13.490738
vtail_sweep=0.000000
vtail_pos_lon=-14.333333
vtail_pos_vert=5.833333
elevator_area=16.250000
aileron_area=11.920000
rudder_area=12.750000
elevator_up_limit=15.000000
elevator_down_limit=15.000000
aileron_up_limit=19.480565
aileron_down_limit=14.896903
rudder_limit=15.000000
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]
//0  Class
//1  Longitudinal Position        (feet)
//2  Lateral Position             (feet)
//3  Vertical Position            (feet)
//4  Impact Damage Threshold      (Feet Per Minute)
//5  Brake Map 		         (0=None, 1=Left, 2=Right)
//6  Wheel Radius	         (feet)
//7  Steer Angle		         (degrees)
//8  Static Compression           (feet)  (0 if rigid)
//9  Max/Static Compression Ratio
//10 Damping Ratio	         (0=Undamped, 1=Critically Damped)
//11 Extension Time	         (seconds)
//12 Retraction Time	         (seconds)
//13 Sound Type
//14 Airspeed limit for retraction (KIAS)
//15 Airspeed that gear gets damage at (KIAS)
point.0=1.000, 15.760, 0.000, -7.260, 1574.803, 0.000, 1.120, 30.000, 0.300, 2.500, 0.453, 5.000, 5.000, 0.000, 0.000, 0.000
point.1=1.000, -2.270, -5.330, -7.260, 1574.803, 1.000, 1.800, 0.000, 0.300, 2.500, 0.627, 5.000, 5.000, 2.000, 0.000, 0.000
point.2=1.000, -2.270, 5.330, -7.260, 1574.803, 2.000, 1.800, 0.000, 0.300, 2.500, 0.627, 5.000, 5.000, 3.000, 0.000, 0.000
point.3=2.000, -15.580, -23.060, -1.250, 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, -15.580, 23.060, -1.250, 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, -15.590, 0.000, -0.330, 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, 5.110, 0.000, -2.990, 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=6.960

[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=8.000000,0.000000
flaps-position.2=20.000000,0.000000
flaps-position.3=40.000000,0.000000

[GeneralEngineData]
engine_type=1
Engine.0=0.000000,-4.910000,0.000000
Engine.1=0.000000,4.910000,0.000000
fuel_flow_scalar=1.000000

[TurbineEngineData]
fuel_flow_gain=0.002170
inlet_area=8.000000
rated_N2_rpm=29920.000000
static_thrust=10000.000000
afterburner_available=0
reverser_available=1

[Reference Speeds]
flaps_up_stall_speed=70.000000
full_flaps_stall_speed=56.000000
cruise_speed=1486.846856

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

[Views]
eyepoint=0.000000,0.000000,0.000000

[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
use_no_default_pitch=1		
use_no_default_bank=1

[direction_indicators]
direction_indicator.0=3,0

[Radios]
// Radio Type=availiable, standby frequency, has glide slope
Audio.1=1
Com.1=1, 0
Com.2=1, 0
Nav.1=1, 0, 1
Nav.2=1, 0, 0
Adf.1=1
Transponder.1=1
Marker.1=1

[LIGHTS]
//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit            
light.0=3,  -15.74, -23.00, -1.31, fx_navred
light.1=3,  -15.74,  23.00, -1.31, fx_navgre
light.2=2,  4.72,   0.00, -2.98, fx_strobe
light.3=1,  -15.03,   0.00, -0.07, fx_beacon
light.4=4,  12.46,   0.00, 1.12, fx_vclight
light.5=4,  7.83,   0.00, 1.12, fx_vclight

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

[jet_engine]
thrust_scalar=1.000

[flight_tuning]
cruise_lift_scalar=1.000
pitch_stability=1.000
roll_stability=1.000
yaw_stability=1.000
parasite_drag_scalar=1.000
induced_drag_scalar=1.000
elevator_effectiveness=1.000
aileron_effectiveness=1.000
rudder_effectiveness=1.000
elevator_trim_effectiveness=1.000
aileron_trim_effectiveness=1.000
rudder_trim_effectiveness=1.000