[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