[fltsim.0]
title=Lun-Spasatel
sim=Lun
model=
panel=
sound=
texture=
checklists=
kb_reference=Lun_ref
description= S.A.R. Ekranoplan "Spasatel", 1989, large Russian heavy duty Air-Sea-Rescue Ground Effect plane in yellow livery, derived from the 1987 "Lun" Missile-Launcher.
ui_manufacturer=Central Hydrofoil Design Bureau
ui_type=Rescue Ekranoplan
ui_variation=S.A.R. Spasatel
atc_id_color=Yellow livery
visual_damage=0

[General]
performance=Length: 240 ft. Span: 144 Ft. Ht: 65 ft\nWeight: 400 Tons\nPower: 8x28,600 ft/lbs Turbojets\nCruising speeds: 243-270 Kts.\nCruising height: 10-25 ft.\nRange: 2000 Km\nMax. Speed: 297 Kts.\nCeiling 24,600 ft\nDesigner: Stephan Scholz, August 2003 
editable=0 

[weight_and_balance]

// ACM V2.0
max_gross_weight = 0
empty_weight = 750000
reference_datum_position = 0, 0, 0
empty_weight_CG_position = 0, 0, 0
empty_weight_pitch_MOI = 90000000
empty_weight_roll_MOI = 4800000
empty_weight_yaw_MOI = 45000000
empty_weight_coupled_MOI = 0
max_number_of_stations =50

station_load.0 =0.000000,0.000000,0.000000,0.000000

[GeneralEngineData]

//0=Piston, 1=Jet, 2=None, 3=Helo-Turbine, 4=Rocket, 5=Turboprop
engine_type = 1
fuel_flow_scalar = 1.000000
engine.0 = 90.000000,-12,6
engine.1 = 90.000000,12,6
engine.2 = 90.000000,-41,6
engine.3 = 90.000000,41,6

[effects]
wake = fx_km_wake
water = fx_km_wave
dirt = fx_tchdrt
concrete = fx_sparks
touchdown = fx_tchdwn_s, 1

[fuel]

//Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)

fuel_type = 2
number_of_tank_selectors = 1

LeftMain = -16.666667, -10.416667, 0, 14242, 0
LeftAux = -25, -31.25, 3.333333, 13243, 0
RightMain = -16.666667, 10.416667, 0, 14242, 0
RightAux = -25, 31.25, 3.333333, 13243, 0


[contact_points]
static_pitch = 0
static_cg_height = 3.1
max_number_of_points = 21

point.0 = 4,-45.7937,72.5,-3.7,9574.80315,0,0,0,9,2.5,0.01802,0,0,6,0,0
point.1 = 4,-45.7827,-72.5,-3.7,9574.80315,0,0,0,9,2.5,0.01802,0,0,5,0,0
point.2 = 4,-25.7937,72.5,-3.7,9574.80315,0,0,0,9,2.5,0.01802,0,0,6,0,0
point.3 = 4,-25.7827,-72.5,-3.7,9574.80315,0,0,0,9,2.5,0.01802,0,0,5,0,0
point.4 = 4,-5.7937,72.5,-3.7,9574.80315,0,0,0,9,2.5,0.01802,0,0,6,0,0
point.5 = 4,-5.7827,-72.5,-3.7,9574.80315,0,0,0,9,2.5,0.01802,0,0,5,0,0
point.6 = 4,15.7937,72.5,-3.7,9574.80315,0,0,0,9,2.5,0.01802,0,0,6,0,0
point.7 = 4,15.7827,-72.5,-3.7,9574.80315,0,0,0,9,2.5,0.01802,0,0,5,0,0
point.8 = 4,87.9648,6.8999,-3.54,9574.80315,0,0,0,5,2.5,0.31802,0,0,2,0,0
point.9 = 4,87.9651,-6.8999,-3.54,9574.80315,0,0,0,5,2.5,0.31802,0,0,3,0,0
point.10 = 4,70.9648,6.8999,-3.54,9574.80315,0,0,0,5,2.5,0.31802,0,0,2,0,0
point.11 = 4,70.9651,-6.8999,-3.54,9574.80315,0,0,0,5,2.5,0.31802,0,0,3,0,0
point.12 = 4,-65.799,6.6997,-3.345,9574.80315,0,0,0,2,2.5,0.31802,0,0,2,0,0
point.13 = 4,-65.799,-6.6997,-3.345,9574.80315,0,0,0,2,2.5,0.31802,0,0,3,0,0
point.14 = 4,-40.799,6.6997,-3.345,9574.80315,0,0,0,2,2.5,0.31802,0,0,2,0,0
point.15 = 4,-40.799,-6.6997,-3.345,9574.80315,0,0,0,2,2.5,0.31802,0,0,3,0,0
point.16 = 4,-82.8211,0,-3.9259,9574.80315,0,0,20,2,2.5,0.31802,0,0,2,0,0
point.17 = 2,-0.63,-68.5,12.9,1574.80315,0,0,0,0,0,0,0,0,5,0,0
point.18 = 2,-0.63,68.5,12.9,1574.80315,0,0,0,0,0,0,0,0,6,0,0
point.19 = 2,-219.6,0.0,70.4651,1574.80315,0,0,0,0,0,0,0,0,9,0,0
point.20 = 2,142.3547,0,9.5218,1574.80315,0,0,0,0,0,0,0,0,4,0,0


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


[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 = 00500
gear_bump_right_duration = 250000
ground_bumps_magnitude1 = 3250
ground_bumps_angle1 = 8900
ground_bumps_intercept1 = 5.0
ground_bumps_slope1 = 0.48
ground_bumps_magnitude2 = 750
ground_bumps_angle2 = 9100
ground_bumps_intercept2 = 0.075
ground_bumps_slope2 = 1.0
crash_magnitude1 = 10000
crash_direction1 = 01000
crash_magnitude2 = 10000
crash_direction2 = 9000
crash_period2 = 75000
crash_duration2 = 2500000

[airplane_geometry]
wing_area = 9615.000000
wing_span = 144
wing_root_chord = 74.91
wing_dihedral = 0.59
wing_incidence = 0.977783
wing_twist = -1.126099
oswald_efficiency_factor = 0.988437
wing_winglets_flag = 0
wing_sweep = 0
wing_pos_apex_lon = 25.82
wing_pos_apex_vert = 0
htail_area = 3550.000000
htail_span = 131
htail_pos_lon = -107
htail_pos_vert = 47
htail_incidence = 0.000000
htail_sweep = 0
vtail_area = 1450.000000
vtail_span = 43.41
vtail_sweep = 0
vtail_pos_lon = -131
vtail_pos_vert = 30
elevator_area = 300.000000
aileron_area = 180.000000
rudder_area = 180.000000
elevator_up_limit = 27.501974
elevator_down_limit = 20.626481
aileron_up_limit = 19.480565
aileron_down_limit = 14.896903
rudder_limit = 23.491270
elevator_trim_limit = 19.480565
spoiler_limit = 59.988681
aileron_to_spoileron_gain = 0.000000
min_ailerons_for_spoilerons = 0.000000
min_flaps_for_spoilerons = 0.000000
spoilerons_available = 0

[electrical]
max_battery_voltage = 24
generator_alternator_voltage = 28
max_generator_alternator_amps = 60
electric_always_available = 0

[Flaps.0]
type=1
span-outboard=0.500000
extending-time=12.000000
system_type=0
flaps-position.0=0.000000,0.000000
flaps-position.1=6.665409,0.000000
flaps-position.2=13.330818,0.000000
flaps-position.3=19.996227,0.000000
flaps-position.4=26.661636,0.000000
flaps-position.5=33.327045,0.000000
flaps-position.6=39.992454,0.000000

[TurbineEngineData]
fuel_flow_gain=0.002170 
inlet_area=68.138120 
rated_N2_rpm=29920
static_thrust=57444
afterburner_available=0 
reverser_available=0 

[jet_engine]
thrust_scalar=1 

[Reference Speeds]
flaps_up_stall_speed=100.000000 
full_flaps_stall_speed=80.000000 
cruise_speed=243.351123 

[Views]
eyepoint=88.005967,0.499815,13.994833


[autopilot]
autopilot_available=1 
flight_director_available=0 
default_vertical_speed=1800.000000 
autothrottle_available=0 
pitch_takeoff_ga=8.000000 

[direction_indicators]
direction_indicator.0=3,0