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#4 |
Master
![]() Registriert seit: 18.02.2001
Beiträge: 604
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![]() Allerdings hab ich den A330-300.
Hier ist der Teil in dem ich Änderungen gemacht habe. Der Reiseflug/Treibstoffverbrauch ist auf FL390 bei Mach:0.82 (260KIAS)optimiert.Falls Du die Verbräuche für den FS-Navigator gebrauchen kannst- sag Bescheid. Sollte das rüberkopieren aus dem Forum nicht klappen- sag Bescheid. Ansonst gilt auch das was mk116 geschrieben hat. Gruss, Wolfgang [General] performance=Passengers\n2-class conf: 335 \n1-class conf: 440\n\nCargo\n32\/33 LD3 containers \/ 11 Pallets \n600 cubic Ft (17 cubic m)\nTotal lower hold volume: 5,656 cu ft \n\nDimensions\nSpan 197 ft 10 in\nLength 208 ft 11 in\nHeight 54 ft 11 in \n\nEngines: PW4000\nTO Thrust Rating: 68,000 lb\n\nMax Fuel Cap.: 24,700 gal\nMaxTOW: 467,400 lb\nZFW: 354,700 lb\n\nMax Range: 4,750 nm\nTypical Cruise Speed \n @ FL350: M.82 atc_type=AIRBUS atc_model=A330 [WEIGHT_AND_BALANCE] reference_datum_position=0.000, 0.000, 0.000 empty_weight_CG_position=0.000, 0.000, 0.000 max_number_of_stations=50 station_load.0=0.000000,0.000000,0.000000,0.000000 empty_weight=354700.000 empty_weight_roll_MOI=8955743.000 empty_weight_pitch_MOI=22600873.000 empty_weight_yaw_MOI=22751035.000 empty_weight_coupled_MOI=1000.000 max_gross_weight=515700.000 CG_forward_limit=0.000 CG_aft_limit=1.000 [flight_tuning] cruise_lift_scalar=1.000 parasite_drag_scalar=1.853 induced_drag_scalar=0.703 elevator_effectiveness=1.205 aileron_effectiveness=1.500 rudder_effectiveness=2.502 pitch_stability=1.405 roll_stability=1.000 yaw_stability=1.000 elevator_trim_effectiveness=1.000 aileron_trim_effectiveness=1.000 rudder_trim_effectiveness=1.000 [pitot_static] vertical_speed_time_constant=999 //Increasing this value will cause a more instantaneous reaction in the VSI [fuel] Center1=0.000, 0.000, -4.000, 16260.000, 3.000 //Center2=-83.676, 0.000, 0.000, 1617.000, 3.000 LeftMain=-7.000, -37.983, 0.000, 3776.000, 3.000 LeftAux=-13.000, -70.269, 0.000, 974.000, 3.000 RightMain=-7.000, 37.983, 0.000, 3776.000, 3.000 RightAux=-13.000, 70.269, 0.000, 974.000, 3.000 fuel_type=2.000 //Fuel type: 1 = Avgas, 2 = JetA number_of_tank_selectors=1 [airplane_geometry] wing_area=3892.000 wing_span=197.833 wing_root_chord=20.000 wing_dihedral=6.218 wing_incidence=0.000 wing_twist=-0.500 oswald_efficiency_factor=0.600 wing_winglets_flag=1 wing_sweep=30.000 wing_pos_apex_lon=25.000 wing_pos_apex_vert=0.000 htail_area=1050.000 htail_span=69.700 htail_pos_lon=-89.200 htail_pos_vert=0.000 htail_incidence=0.000 htail_sweep=40.000 vtail_area=690.000 vtail_span=27.300 vtail_sweep=35.000 vtail_pos_lon=-83.676 vtail_pos_vert=5.800 elevator_area=137.000 aileron_area=68.000 rudder_area=232.000 elevator_up_limit=24.000 elevator_down_limit=18.000 aileron_up_limit=25.000 aileron_down_limit=25.000 rudder_limit=45.000 elevator_trim_limit=15.000 spoiler_limit=35.000 spoilerons_available=0 aileron_to_spoileron_gain=3.000 min_ailerons_for_spoilerons=9.969 min_flaps_for_spoilerons=0.000 [GeneralEngineData] engine_type=1 Engine.0=15.166, -30.386, -7.583 Engine.1=15.166, 30.386, -7.583 fuel_flow_scalar=0.497 [TurbineEngineData] bypass_ratio=5.00 fuel_flow_gain=0.001 inlet_area=54.522 rated_N2_rpm=29922.000 static_thrust=68000.000 afterburner_available=0 reverser_available=1 [jet_engine] thrust_scalar=1.101 [Reference Speeds] flaps_up_stall_speed=132.000 full_flaps_stall_speed=124.000 cruise_speed=460.000 [keyboard_response] elevator=100.000, 200.000 aileron=100.000, 200.000 rudder=50.000, 100.000 [Views] eyepoint=78.502, -1.756, 9.628 [autopilot] autopilot_available=1 flight_director_available=1 default_vertical_speed=1800.000 autothrottle_available=1 autothrottle_arming_required=1 autothrottle_takeoff_ga=1 autothrottle_max_rpm=105.000 pitch_takeoff_ga=8.000 use_no_default_pitch=1 // 0 = Default to current pitch mode, 1 = No default pitch mode. use_no_default_bank=1 // 0 = Default to Wing Leveler mode, 1 = No default bank mode. [direction_indicators] direction_indicator.0=3,0 |
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