[fltsim.0]
title=LRHS Business Jet
sim=stcr1250
model=
panel=
sound=
texture=
checklists=
ui_manufacturer=JasTek Aerospace
ui_type=LRHSBJ-1
ui_variation=White w/Blue Stripes
description=Long Range High Speed Business Jet.\nConcept aircraft. 
atc_heavy=0
atc_id=N1701E
atc_airline=
atc_flight_number=



[fltsim.1]
title=LRHS Business Jet (Red)
sim=stcr1250
model=
panel=
sound=
texture=1
checklists=
ui_manufacturer=JasTek Aerospace
ui_type=LRHSBJ-1
ui_variation=White w/Red Stripes
description=Long Range High Speed Business Jet.\nConcept aircraft.
atc_heavy=0
atc_id=N1701E
atc_airline=
atc_flight_number=


[fltsim.2]
title=LRHS Business Jet (Gold)
sim=stcr1250
model=
panel=
sound=
texture=2
checklists=
ui_manufacturer=JasTek Aerospace
ui_type=LRHSBJ-1
ui_variation=White w/Gold Stripes
description=Long Range High Speed Business Jet.\nConcept aircraft.
atc_heavy=0
atc_id=N1701E
atc_airline=
atc_flight_number=


[fltsim.3]
title=LRHS Business Jet (Green)
sim=stcr1250
model=
panel=
sound=
texture=3
checklists=
ui_manufacturer=JasTek Aerospace
ui_type=LRHSBJ-1
ui_variation=White w/Green Stripes
description=Long Range High Speed Business Jet.\nConcept aircraft.
atc_heavy=0
atc_id=N1701E
atc_airline=
atc_flight_number=


[forcefeedback]
stick_shaker_magnitude=5000		; 0 - 10000
stick_shaker_direction=0		; 0 - 35999 degrees
stick_shaker_period=111111		; in microseconds
gear_bump_nose_magnitude=3000		; 0 - 10000
gear_bump_nose_direction=18000		; 0 - 35999 degrees
gear_bump_nose_duration=250000		; in microseconds
gear_bump_left_magnitude=2700		; 0 - 10000
gear_bump_left_direction=9000		; 0 - 35999 degrees
gear_bump_left_duration=250000		; in microseconds
gear_bump_right_magnitude=2700		; 0 - 10000
gear_bump_right_direction=27000		; 0 - 35999 degrees
gear_bump_right_duration=250000		; in microseconds
ground_bumps_magnitude1=1300		; 0 - 10000
ground_bumps_angle1=08900		; 0 - 35999 degrees
ground_bumps_intercept1=3.0
ground_bumps_slope1=0.20
ground_bumps_magnitude2=200		; 0 - 10000
ground_bumps_angle2=09100		; 0 - 35999 degrees
ground_bumps_intercept2=1.075
ground_bumps_slope2=0.035
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
[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= 12000.000
empty_weight_roll_MOI= 17680.000
empty_weight_pitch_MOI= 19694.000
empty_weight_yaw_MOI= 37484.000
empty_weight_coupled_MOI= 0.000
max_gross_weight= 18003.200
CG_forward_limit= 0.000
CG_aft_limit= 1.000
[fuel]
Center1= -6.860, 0.000, -1.500, 359.000, 0.000
LeftMain= -1.800, -10.000, -1.500, 268.500, 0.000
RightMain= -1.800, 10.000, -1.500, 268.500, 0.000
fuel_type= 2.000
number_of_tank_selectors= 1
[airplane_geometry]
wing_area               = 310.000
wing_span               = 45.000
wing_root_chord         = 6.900
wing_dihedral           = 6.000
wing_incidence          = 1.000
wing_twist              = -1.500
oswald_efficiency_factor= 0.700
wing_winglets_flag      = 1
wing_sweep              = 15.000
wing_pos_apex_lon       = 2.100
wing_pos_apex_vert      = 0.000
htail_area              = 67.000
htail_span              = 17.200
htail_pos_lon           = -22.600
htail_pos_vert          = 0.000
htail_incidence         = 0.500
htail_sweep             = 20.000
vtail_area              = 42.000
vtail_span              = 7.400
vtail_sweep             = 40.000
vtail_pos_lon           = -20.500
vtail_pos_vert          = 4.100
elevator_area           = 17.000
aileron_area            = 13.500
rudder_area             = 7.300
elevator_up_limit       = 17.000
elevator_down_limit     = 15.500
aileron_up_limit        = 18.000
aileron_down_limit      = 18.000
rudder_limit            = 30.000
elevator_trim_limit     = 15.000
spoiler_limit           = 30.000
spoilerons_available    = 1
aileron_to_spoileron_gain = 3.000
min_ailerons_for_spoilerons = 10.000
min_flaps_for_spoilerons = 0.000

[Reference Speeds]
flaps_up_stall_speed    = 96.000
full_flaps_stall_speed  = 76.800
cruise_speed            = 315.000




[contact_points]
point.0= 1.000, 23.333, 0.000, -4.417, 1181.102, 0.000, 0.625, 46.800, 0.418, 2.500, 0.589, 5.000, 5.000, 0.000, 0.000, 0.000
point.1= 1.000, -2.750, -4.750, -4.917, 1574.803, 1.000, 0.625, 0.000, 0.440, 2.500, 0.570, 5.000, 5.000, 2.000, 0.000, 0.000
point.2= 1.000, -2.750, 4.750, -4.917, 1574.803, 2.000, 0.625, 0.000, 0.440, 2.500, 0.570, 5.000, 5.000, 3.000, 0.000, 0.000
point.3= 2.000, -3.333, -23.917, -3.000, 787.402, 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, -3.333, 23.917, -3.000, 787.402, 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, -22.667, 0.000, 0.000, 787.402, 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, 23.083, 0.000, -1.500, 787.402, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 4.000, 0.000, 0.000
static_pitch= -0.753
static_cg_height= 4.409
[GeneralEngineData]
engine_type= 1
Engine.0= -8.333, -4.833, 0.833
Engine.1= -8.333, 4.833, 0.833
fuel_flow_scalar= 0.350
[TurbineEngineData]
fuel_flow_gain= 0.100
inlet_area= 4.290
rated_N2_rpm= 29920.000
static_thrust= 3375.000
afterburner_available= 0
reverser_available= 1
[Reference Speeds]
flaps_up_stall_speed= 100.000
full_flaps_stall_speed= 80.000
cruise_speed= 1442.356
[keyboard_response]
elevator= 150.000, 250.000
aileron= 150.000, 250.000
rudder= 150.000, 250.000
[Views]
eyepoint= 17.391, -1.307, 5.998
[General]
performance=Max Cruise:  1000 kts (Mach 1.55)\nThrust:  3,375 lb x 2\nMax Range: 5,500 nm\nCeiling: 50,000ft\nPassengers:  8\nDesigner:  James A. Smith\nDate:  11\/2002
atc_type=
atc_model=LRHSBJ-1
[autopilot]
autopilot_available= 1
flight_director_available= 1
default_vertical_speed= 2000.000
autothrottle_available= 1
autothrottle_arming_required= 1
autothrottle_takeoff_ga= 1
autothrottle_max_rpm= 90.000
pitch_takeoff_ga= 8.000
[direction_indicators]
direction_indicator.0=3,0
[jet_engine]
thrust_scalar=1.651
[flight_tuning]
cruise_lift_scalar=1.000
pitch_stability=2.002
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=1.500
aileron_trim_effectiveness=1.000
rudder_trim_effectiveness=1.000
[Flaps.0]
type= 1
span-outboard= 0.500
extending-time= 5.000
system_type= 0
damaging-speed= 0.000
blowout-speed= 0.000
lift_scalar= 1.000
drag_scalar= 1.000
pitch_scalar= 1.000
flaps-position.0= 0.000, 0.000
flaps-position.1= 13.331, 0.000
flaps-position.2= 26.662, 0.000
flaps-position.3= 39.992, 0.000