[fltsim.0]
title=LS-8-18
sim=LS8-18
model=
panel=
sound=
texture=
texture=
kb_reference=LS-8_ref
kb_checklists=LS-8_check
ui_manufacturer=Rolladen-Schneider
ui_type=LS 8-18
ui_variation=White and Blue
description=The Rolladen-Schneider LS8-18 is a standard class glider with an extended wingspan and winglets. It was designed and originally produced by Rolladen-Schneider. It is currently manufactured by DG Flugzeugbau.
atc_id=D0442
visual_damage=1
[General]
atc_type=Schneider
atc_model=LS8
performance=Wingspan: 18 m\nEmpty weight: 265 kg\nRate of sink: 0,50 m/s\nMaximum speed: 280 km/h
[electrical]
max_battery_voltage=24
avionics_bus=0, 0 , 0
avionics=0, 0 , 0
additional_system=0, 0 , 0
flap_motor=0, 0 , 0
gear_motor=0, 0 , 0
[WEIGHT_AND_BALANCE]
reference_datum_position=0,0,0
empty_weight_CG_position=-2.0,0,0
max_number_of_stations=5
station_load.0="170, 0.8,0,0,Pilot"
station_load.1="170, -1.000,0,0,Ballast"
empty_weight=540.000000
empty_weight_roll_MOI=900.000000
empty_weight_pitch_MOI=900.000000
empty_weight_yaw_MOI=1000.000000
empty_weight_coupled_MOI=0.000000
max_gross_weight=1191.000000
[flight_tuning]
//Speed Polars (wet) checked (only for FS9): August 2005
cruise_lift_scalar=0.8
parasite_drag_scalar=0.65
induced_drag_scalar=1.2
elevator_effectiveness=1.0
aileron_effectiveness=1.1
rudder_effectiveness=0.8
pitch_stability=1.0
roll_stability=1.0
yaw_stability=1.0
elevator_trim_effectiveness=1.3
aileron_trim_effectiveness=1.0
rudder_trim_effectiveness=1.00
[airplane_geometry]
wing_area=125.000000
wing_span=59
wing_root_chord=3.2
wing_dihedral=3
wing_incidence=3
wing_twist=1
oswald_efficiency_factor=0.8
wing_winglets_flag=1
wing_sweep=0.000000
wing_pos_apex_lon=0.000
wing_pos_apex_vert=2
htail_area=12.500000
htail_span=8
htail_pos_lon=-11.5
htail_pos_vert=5.8000000
htail_incidence=2.0
htail_sweep=0.000000
vtail_area=6
vtail_span=3
vtail_sweep=0.000000
vtail_pos_lon=-12
vtail_pos_vert=2
elevator_area=6
aileron_area=11.900000
rudder_area=3
elevator_up_limit=18
elevator_down_limit=15
aileron_up_limit=20
aileron_down_limit=10
rudder_limit=23.491270
elevator_trim_limit=70
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
auto_spoiler_available=0
spoiler_extension_time=0.500000
positive_g_limit_flaps_up=5.500000
positive_g_limit_flaps_down=5.500000
negative_g_limit_flaps_up=-3.500000
negative_g_limit_flaps_down=-3.500000
[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
// Lang. Breit. Vert.
// Pos. Pos. Pos.
// 0 1 2 3 4 5 6 7 8 9 10 11 12 13 14 15
//--------------------------------------------------------------------------------------------------------------------------------
point.0=1, -13.0, 0, 0.71, 1574.8, 0, 0.5062, 85, 0.3, 2.5, 0.35, 0.6, 0.6, 0, 0, 0 // Gear Tail
point.1=1, 0.8, 0.0, -2.19, 1574.8, 1, 0.509, 0, 0.4, 2.5, 0.50, 0.6, 0.6, 2, 0, 0 // Gear Main
point.2=2, 0.44, -28, 3.3, 1574.4, 0, 0, 0, 0, 0, 0, 0, 0, 5, 0, 0 // Wing Tip
point.3=2, 0.44, 28, 3.3, 1574.4, 0, 0, 0, 0, 0, 0, 0, 0, 6, 0, 0 // Wing Tip
point.4=2, -12.4, 0, 0.7, 1574.4, 0, 0, 0, 0, 0, 0, 0, 0, 9, 0, 0 // Tail
point.5=2, 4.3, 0, -1.50, 1574.4, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0 // Nose
//Converted with CPA V.1.05 by Wolfgang Piper
static_pitch=10.0
static_cg_height=1.80
gear_system_type=0
[Views]
eyepoint=2.42,0, 1.13
[GeneralEngineData]
engine_type=1
Engine.0=-2,0,0
fuel_flow_scalar=3.400000
min_throttle_limit=0.000000
[TurbineEngineData]
fuel_flow_gain=0.002170
inlet_area=1
rated_N2_rpm=29920.000000
static_thrust=580
afterburner_available=0
reverser_available=0
[jet_engine]
thrust_scalar=1.000
[fuel]
Center1=0.000000,0.000000,0.000000,1.000000,9.000000
fuel_type=2.000000
number_of_tank_selectors=1
electric_pump=0
[Reference Speeds]
flaps_up_stall_speed=35.000000
full_flaps_stall_speed=34.00000
cruise_speed=45.0000
max_indicated_speed=250
max_mach=0.260010
[keyboard_response]
elevator=60.000000,90.000000
aileron=60.000000,90.000000
rudder=60.000000,90.000000
[autopilot]
autopilot_available=0
flight_director_available=0
[direction_indicators]
direction_indicator.0=0,0
[brakes]
toe_brakes_scale=0.7
parking_brake=1
[gear_warning_system]
gear_warning_available=0
pct_throttle_limit=0.000000
flap_limit_power=0.000000
flap_limit_idle=0.000000
[hydraulic_system]
normal_pressure=0.000000
[stall_warning]
type=1
stick_shaker=0
[attitude_indicators]
attitude_indicator.0=1
[turn_indicators]
turn_indicator.0=1,0
[Flaps.0]
type=0
span-outboard=0.500000
extending-time=0.000000
system_type=0
[exits]
number_of_exits=2
exit_rate.0=0.2
[forcefeedback]
gear_bump_nose_magnitude = 6000
gear_bump_nose_direction = 18000
gear_bump_nose_duration = 250000
gear_bump_left_magnitude = 6000
gear_bump_left_direction = 35500
gear_bump_left_duration = 250000
gear_bump_right_magnitude = 6000
gear_bump_right_direction = 500
gear_bump_right_duration = 250000
ground_bumps_magnitude1 = 3250
ground_bumps_angle1 = 8900
ground_bumps_intercept1 = 5#
ground_bumps_slope1 = 0.48
ground_bumps_magnitude2 = 750
ground_bumps_angle2 = 9100
ground_bumps_intercept2 = 0.075
ground_bumps_slope2 = 1#
crash_magnitude1 = 10000
crash_direction1 = 1000
crash_magnitude2 = 10000
crash_direction2 = 9000
crash_period2 = 75000
crash_duration2 = 2500000
[pitot_static]
pitot_heat=0.000000
[vacuum_system]
max_pressure=5.000000
vacuum_type=1
electric_backup_pressure=0.000000
engine_map=1,1,1,1
[pneumatic_system]
max_pressure=0.000000
bleed_air_scalar=0.000000
[deice_system]
structural_deice_type=0
[EFFECTS]
wake=fx_wake
water=fx_spray
dirt=fx_tchdrt
concrete=fx_sparks
touchdown=fx_tchdwn_s, 1