[fltsim.0] title=Grob Twin III Acro 9 sim=grob3t model= panel= sound= texture= ui_manufacturer=Grob ui_type=Twin III Acro ui_variation=VC front-rear description=Fly from the front seat - with towed simulation... atc_heavy=0 atc_id= atc_airline= atc_flight_number= atc_id_color=0000000000 visual_damage=0 [General] performance= atc_type= atc_model= editable=0 [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] max_gross_weight = 1680 empty_weight = 1160 reference_datum_position = 0, 0, 0 empty_weight_CG_position = 0, 0, 0 empty_weight_pitch_MOI = 1700 empty_weight_roll_MOI = 2300 empty_weight_yaw_MOI = 1800 empty_weight_coupled_MOI = 0 max_number_of_stations =50 station_load.0 =0.000000,0.000000,0.000000,0.000000 [fuel] //Tanks Position and capacity: //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons) LeftMain = 0, 0, 0.00, 0.25, 0.00 RightMain= 0, 0, 0.00, 0.25, 0.00 //Fuel type: 1 = Avgas, 2 = JetA fuel_type=1 number_of_tank_selectors = 1 electric_pump=1 [GeneralEngineData] engine_type = 0 //0=Piston, 1=Jet, 2=None, 3=Helo-Turbine, 4=Rocket, 5=Turboprop Engine.0 = 2.4, 0.0, 0.0 //(feet) longitudinal, lateral, vertical distance from reference datum fuel_flow_scalar= 1.0 //Fuel flow scalar min_throttle_limit = 0.0 //Minimum percent throttle. Generally negative for turbine reverser [piston_engine] power_scalar = 1.0 //Piston power scalar cylinder_displacement= 90.0 //Cubic inches per cylinder compression_ratio= 8.5 //Compression ratio number_of_cylinders=2 //Number of cylinders max_rated_rpm= 1575 //Max rated RPM max_rated_hp= 50 //Max rated HP fuel_metering_type= 1 //0=Fuel Injected, 1=Gravity Carburetor, 2=Aerobatic Carburetor cooling_type= 0 //0=Cooling type Air, 1=Cooling type Liquid normalized_starter_torque= 0.5 //Starter torque factor turbocharged= 0 //Is it turbocharged? 0=FALSE, 1=TRUE max_design_mp= 35 //Max design manifold pressure, (inHg) min_design_mp= 0 //Min design manifold pressure, (inHg) critical_altitude= 24000.00 //Altitude to which the turbocharger will provide max design manifold pressure (feet) emergency_boost_type= 0 //0=None, 1=Water Injection, 2=Methanol/Water injection, 3=War Emergency Power emergency_boost_mp_offset= 0 //Additional manifold pressure supplied by emergency boost emergency_boost_gain_offset= 0 //Multiplier on manifold pressure due to emergency boost fuel_air_auto_mixture= 1 //Automixture available? 0=FALSE, 1=TRUE auto_ignition= 0 //Auto-Ignition available? 0=FALSE, 1=TRUE max_rpm_mechanical_efficiency_scalar= 1.0 //Scalar on maximum RPM mechanical efficiency idle_rpm_mechanical_efficiency_scalar= 1.0 //Scalar on idle RPM mechanical efficiency max_rpm_friction_scalar= 1.0 //Scalar on maximum RPM friction idle_rpm_friction_scalar= 1.0 //Scalar on idle RPM friction [propeller] thrust_scalar = 1.0 //Propeller thrust scalar propeller_type= 0 //0=Constant Speed, 1=Fixed Pitch propeller_diameter= 6.58 //Propeller Diameter, (feet) propeller_blades= 3 //Number of propeller blades propeller_moi= 8.3 //Propeller moment of inertia beta_max= 31.7 //Maximum blade pitch angle for constant speed prop, (degrees) beta_min= 14.9 //Minimum blade pitch angle for constant speed prop, (degrees) min_gov_rpm= 1400 //Miminum governed RPM prop_tc= 0.1 //Prop time-constant gear_reduction_ratio= 1.0 //Propeller gear reduction ratio fixed_pitch_beta= 20 //Fixed pitch angle of fixed pitch prop, (degrees) low_speed_theory_limit= 80 //Speed at which low speed theory becomes blended in (feet/second) prop_sync_available= 0 //Prop synchronization available? 0=FALSE, 1=TRUE prop_deice_available= 0 //Prop de-icing available? 0=FALSE, 1=TRUE prop_feathering_available= 0 //Prop feathering available? 0=FALSE, 1=TRUE prop_auto_feathering_available= 0 //Prop auto-feathering available? 0=FALSE, 1=TRUE min_rpm_for_feather= 0 //Minimum RPM for prop feathering beta_feather= 0 //Feathering pitch angle (degrees) power_absorbed_cf= 0 //Coefficient of friction for power absorbed by propeller defeathering_accumulators_available= 0 //Defeathering accumulators available? 0=FALSE, 1=TRUE prop_reverse_available= 0 //Prop reverse available? 0=FALSE, 1=TRUE minimum_on_ground_beta= 0 //Miminum pitch angle on ground, (degrees) minimum_reverse_beta= 0 //Minimum pitch angle in reverse, (degrees) [contact_points] static_cg_height = 2 max_number_of_points = 6 point.0 = 1, -14.4, 0, -2.1, 1575, 0, 0.507, 0, 0.417, 2.5, 0.611, 0, 0, 0, 0, 0 point.1 = 1, 1.167, 0.083, -2, 1575, 1, 0.5, 0, 0.278, 2.5, 0.865, 0, 0, 2, 0, 0 point.2 = 1, 1.167, -0.083, -2, 1575, 2, 0.5, 0, 0.278, 2.5, 0.865, 0, 0, 3, 0, 0 point.3 = 2, 0, -29.5, 1.9, 1575, 0, 0, 0, 0, 0, 0, 0, 0, 5, 0, 0 point.4 = 2, 0, 29.5, 1.9, 1575, 0, 0, 0, 0, 0, 0, 0, 0, 6, 0, 0 point.5 = 2, 6.9, 0, 0, 1575, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0 static_pitch=0.000000 [keyboard_response] elevator = 150.000000, 250.000000 aileron = 150.000000, 250.000000 rudder = 150.000000, 250.000000 [forcefeedback] [airplane_geometry] wing_area=192.000000 wing_span=57.333333 wing_root_chord=3.333333 wing_dihedral=3.499146 wing_incidence=0.000000 wing_twist=0.999756 oswald_efficiency_factor=0.793795 wing_winglets_flag=0 wing_sweep=0.000000 wing_pos_apex_lon=0.000000 wing_pos_apex_vert=0.000000 htail_area=25.000000 htail_span=6.333333 htail_pos_lon=-16.416667 htail_pos_vert=0.000000 htail_incidence=0.000000 htail_sweep=0.000000 vtail_area=32.000000 vtail_span=6.449806 vtail_sweep=0.000000 vtail_pos_lon=-14.750000 vtail_pos_vert=3.916667 elevator_area=9.460000 aileron_area=11.900000 rudder_area=7.700000 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 spoilerons_available=0 aileron_to_spoileron_gain=0.000000 min_ailerons_for_spoilerons=0.000000 min_flaps_for_spoilerons=0.000000 [Reference Speeds] flaps_up_stall_speed=40.000 full_flaps_stall_speed=32.000 cruise_speed=71.088 max_indicated_speed=180.734375 max_mach=0.329980 [Views] eyepoint=4.68, 0.0, 1.40 // viewpoint front-seat [autopilot] autopilot_available=0 flight_director_available=0 [direction_indicators] direction_indicator.0=0,0 [flight_tuning] cruise_lift_scalar=1.000 pitch_stability=1.000 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=1.000 aileron_trim_effectiveness=1.000 rudder_trim_effectiveness=1.000 [brakes] toe_brakes_scale=1.000031 parking_brake=1 [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
