[fltsim.0] title=G-102 Astir CS FAC sim=Grob G-102 Astir CS model= panel= sound= texture= ui_manufacturer=Grob ui_type=G-102 Astir CS Light ui_variation=Fuerza Aérea Colombiana kb_checklists= kb_reference= description= visual_damage=0 atc_id_color=000000 [General] performance= atc_type= atc_model= editable=0 [WEIGHT_AND_BALANCE] max_gross_weight = 1000 // (pounds) empty_weight = 800 // (pounds) reference_datum_position = 1.25, 0, 0 // (feet) distance from FlightSim Reference position: (1/4 chord, centerline, waterline) empty_weight_CG_position = -1.00, 0, 0 // (feet) longitudinal, lateral, vertical distance from specified datum max_number_of_stations = 50 station_load.0 = "170, -0.8, 0.0, 0.0, Pilot" // Weight (lbs), longitudinal, lateral, vertical positions from datum (feet) ;Moments of Inertia empty_weight_pitch_MOI = 1800 empty_weight_roll_MOI = 2400 empty_weight_yaw_MOI = 1800 empty_weight_coupled_MOI = 0.0 [contact_points] static_pitch = 7.4 static_cg_height = 2 max_number_of_points = 6 point.0 = 1, -13.2, 0, -0.6, 1575, 0, 0.3, 0, 0.417, 2.5, 0.611, 0, 0, 0, 0, 0 point.1 = 1, 0.5, 0.1, -2.3, 1575.0, 1.0, 0.5, 0.0, 0.278, 2.5, 0.865, 3.0, 3.0, 2.0, 0.0, 0.0 point.2 = 1, 0.5, -0.1, -2.3, 1575.0, 1.0, 0.5, 0.0, 0.278, 2.5, 0.865, 3.0, 3.0, 2.0, 0.0, 0.0 point.3 = 2, 0.0, -24.5, 1.0, 1575.0, 0.0, 0.0, 0.0, 0.000, 0.0, 0.000, 0.0, 0.0, 5.0, 0.0, 0.0 point.4 = 2, 0.0, 24.5, 1.0, 1575.0, 0.0, 0.0, 0.0, 0.000, 0.0, 0.000, 0.0, 0.0, 6.0, 0.0, 0.0 point.5 = 2, 4.0, 0.0, -1.7, 1575.0, 0.0, 0.0, 0.0, 0.000, 0.0, 0.000, 0.0, 0.0, 0.0, 0.0, 0.0 gear_system_type=0 [keyboard_response] elevator = 60.000000, 90.000000 aileron = 60.000000, 90.000000 rudder = 60.000000, 90.000000 [forcefeedback] [EFFECTS] wake=fx_wake water=fx_spray dirt=fx_tchdrt startup=fx_dummy touchdown = fx_tchdwn, 1 [airplane_geometry] wing_area = 180.0 //Square feet wing_span = 57.0 //Feet wing_root_chord = 4.6 //Feet wing_dihedral = 3.5 //Degrees wing_incidence = 3.0 //Degrees wing_twist = -2.0 //Degrees oswald_efficiency_factor= 1.0 //Measure of lift effeciency of wing wing_winglets_flag = 0 //Are winglets available? wing_sweep = 0.0 //Degrees, wing leading edge wing_pos_apex_lon = -0.5 //Feet, longitudinal distance from reference point, negative going aft wing_pos_apex_vert = 0.0 //Feet, vertical distance from reference point, positive going up htail_area = 21.0 //Square feet htail_span = 7.9 //Feet htail_pos_lon = -17.3 //Feet, longitudinal distance from reference point, negative going aft htail_pos_vert = 0.0 //Feet, vertical distance from reference point, positive going up htail_incidence = 0.0 //Degrees htail_sweep = 0.0 //Degrees, horizontal tail leading edge vtail_area = 17.0 //Square feet vtail_span = 4.7 //Feet, tip to body vtail_sweep = 0.0 //Degrees, vertical tail leading edge vtail_pos_lon = -16.0 //Feet, longitudinal distance from reference point, negative going aft vtail_pos_vert = 3.9 //Feet, vertical distance from reference point, positive going up elevator_area = 16.0 //Square feet aileron_area = 14.7 //Square feet rudder_area = 26.0 //Square feet elevator_up_limit = 26.0 //Degrees elevator_down_limit = 26.0 //Degrees aileron_up_limit = 30.0 //Degrees aileron_down_limit = 30.0 //Degrees rudder_limit = 30.0 //Degrees elevator_trim_limit = 15.0 //Degrees spoiler_limit = 90.00 //Degrees spoilerons_available = 0 //Spoilerons Available? aileron_to_spoileron_gain = 0 //Aileron to spoileron gain min_ailerons_for_spoilerons = 0 //Degrees min_flaps_for_spoilerons = 0 //Minimum flap handle position when spoilerons activate [electrical] max_battery_voltage = 24 generator_alternator_voltage = 28 max_generator_alternator_amps = 60 electric_always_available = 0 flap_motor = 0, 0, 0 gear_motor = 0, 0, 0 avionics_bus = 0, 0, 0 avionics = 0, 0, 0 additional_system = 0, 0, 0 [flight_tuning] cruise_lift_scalar = 1.0 parasite_drag_scalar = 0.1 induced_drag_scalar = 0.1 elevator_effectiveness = 1.0 aileron_effectiveness = 1.0 rudder_effectiveness = 0.3 pitch_stability = 1.5 roll_stability = 1.0 yaw_stability = 1.0 elevator_trim_effectiveness = 1.0 aileron_trim_effectiveness = 1.0 rudder_trim_effectiveness = 1.0 [Reference Speeds] flaps_up_stall_speed = 40.0 //Knots True (KTAS) full_flaps_stall_speed = 40.0 //Knots True (KTAS) cruise_speed = 47.0 //Knots True (KTAS) max_indicated_speed = 158 //Red line (KIAS) max_mach=0.229980 [Views] eyepoint=1.35, 0.0, 0.77 [autopilot] autopilot_available=0 flight_director_available=0 [direction_indicators] direction_indicator.0=0,0 [brakes] toe_brakes_scale=1.000031 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 [Flaps.0] type=0 span-outboard=0.500000 extending-time=0.000000 system_type=0 [hydraulic_system] normal_pressure=0.000000 [stall_warning] type=1 [attitude_indicators] attitude_indicator.0=1 [turn_indicators] turn_indicator.0=1,0 [TurbineEngineData] fuel_flow_gain = 0.002 inlet_area = 12.018 rated_N2_rpm = 29920.000 static_thrust = 1700.000 afterburner_available = 0 reverser_available = 0 [GeneralEngineData] engine_type = 1 fuel_flow_scalar = 0.2 // 1.000 engine.0 = 0.000, 0.000, 0.000 min_throttle_limit=0.000000 [fuel] fuel_type = 2 number_of_tank_selectors = 1 Center1 = 0, 0, 0, 1, 0 LeftMain = 0, 0, 0, 11.9, 0 RightMain = 0, 0, 0, 11.9, 0 electric_pump=0 [smokesystem] smoke.0 = 20.00, -10.0, 0.0, fx_water_ballast
