// A-ST SST2010 Europe by Shigeru Tanaka // Swing-wing SST2010 for Air France, Lufthansa, and British Airways [fltsim.0] title=A-ST SST2010 sim=A-ST SST2010 model= panel= sound= texture= checklists= ui_manufacturer=A-ST SST2010 Europe ui_type=A-ST SST2010 British Airways ui_variation=SST2010 for British Airways description=An innovative conceptual model of Super Sonic Transport for 2010 in British Airways livery. Futuristic design with swing-wing configuration and luxurious mach 2 crusing speed. Original model by Shigeru Tanaka. atc_heavy=1 atc_id=G2010 atc_airline=British Airways atc_flight_number=G2010 [fltsim.1] title=A-ST SST2010 paint2 sim=A-ST SST2010 model=1 panel= sound= texture=1 checklists= ui_manufacturer=A-ST SST2010 Europe ui_type=A-ST SST2010 Lufthansa ui_variation=Supersonik Flugzeug fur Lufthansa description=Ein naechste Generation Super Sonik Flugzeug SST2010 ab Jahr 2010 mit Geschwindigkeit Mach 2 in der Deutschen Lufthansa Farben. Origineller Idee, Modell, Design und farbliche Ausstattung von Shigeru Tanaka. atc_heavy=1 atc_id=D2010 atc_airline=Lufthansa atc_flight_number=D2010 [fltsim.2] title=A-ST SST2010 paint3 sim=A-ST SST2010 model=1 panel= sound= texture=2 checklists= description=Ce modele futuriste de haute qualite, SST2010. Annee 2010, une nouvelle generation de supersonic aux couleurs de la Air France. Operationnelles vitesse mach 2. Realisation originale de Shigeru Tanaka. Bon voyage. ui_manufacturer=A-ST SST2010 Europe ui_type=A-ST SST2010 Air France ui_variation=Nouvelle Generation de Supersonic atc_heavy=1 atc_id=F2010 atc_airline=Air France atc_flight_number=F2010 [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=234567.000 empty_weight_roll_MOI=10431175.000 empty_weight_pitch_MOI=20779505.000 empty_weight_yaw_MOI=19237558.000 empty_weight_coupled_MOI=1300.000 max_gross_weight=401772.195 CG_forward_limit=0.000 CG_aft_limit=1.000 [flight_tuning] cruise_lift_scalar = 1.0 parasite_drag_scalar = 1.0 induced_drag_scalar = 1.0 elevator_effectiveness = 1.0 aileron_effectiveness = 1.0 rudder_effectiveness = 1.0 pitch_stability = 1.0 roll_stability = 1.0 yaw_stability = 1.0 elevator_trim_effectiveness = 1.0 aileron_trim_effectiveness = 1.0 rudder_trim_effectiveness = 1.0 [fuel] LeftMain=0.000, 0.000, 0.000, 11728.000, 0.000 LeftAux=0.000, -53.333, 0.000, 750.000, 0.000 RightMain=0.000, 0.000, 0.000, 11728.000, 0.000 RightAux=0.000, 53.333, 0.000, 750.000, 0.000 fuel_type=2.000 number_of_tank_selectors=1 [airplane_geometry] wing_area=2886.000 wing_span=133.417 wing_root_chord=21.667 wing_dihedral=6.998 wing_incidence=0.000 wing_twist=-1.000 oswald_efficiency_factor=0.750 wing_winglets_flag=0 wing_sweep=0.000 wing_pos_apex_lon=0.000 wing_pos_apex_vert=0.000 htail_area=1400.000 htail_span=41.667 htail_pos_lon=-83.333 htail_pos_vert=0.000 htail_incidence=0.000 htail_sweep=0.000 vtail_area=700.000 vtail_span=30.166 vtail_sweep=0.000 vtail_pos_lon=-66.667 vtail_pos_vert=5.833 elevator_area=350.000 aileron_area=115.440 rudder_area=119.000 elevator_up_limit=27.502 elevator_down_limit=20.626 aileron_up_limit=19.481 aileron_down_limit=14.897 rudder_limit=23.491 elevator_trim_limit=19.481 spoiler_limit=59.989 spoilerons_available=0 aileron_to_spoileron_gain=0.000 min_ailerons_for_spoilerons=0.000 min_flaps_for_spoilerons=0.000 [contact_points] point.0=1.000, 48.167, 0.000, -17.34600, 1774.803, 0.000, 3.285, 64.680, 0.470, 2.500, 0.7404, 5.000, 5.000, 0.000, 0.000, 0.000 point.1=1.000, -35.417, -9.167, -17.34600, 1574.803, 1.000, 3.285, 0.000, 0.486, 2.500, 0.7509, 5.000, 5.000, 2.000, 0.000, 0.000 point.2=1.000, -35.417, 9.167, -17.34600, 1574.803, 2.000, 3.285, 0.000, 0.486, 2.500, 0.7509, 5.000, 5.000, 3.000, 0.000, 0.000 point.3=1.000, -40.417, -11.167, -17.34600, 1574.803, 1.000, 3.285, 0.000, 0.486, 2.500, 0.7509, 5.000, 5.000, 2.000, 0.000, 0.000 point.4=1.000, -40.417, 11.167, -17.34600, 1574.803, 2.000, 3.285, 0.000, 0.486, 2.500, 0.7509, 5.000, 5.000, 3.000, 0.000, 0.000 point.5=2.000, -52.417, -58.417, -3.417, 1274.803, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 5.000, 0.000, 0.000 point.6=2.000, -52.417, 58.417, -3.417, 1274.803, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 6.000, 0.000, 0.000 point.7=2.000, 101.167, 0.000, -2.667, 1504.803, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 4.000, 0.000, 0.000 point.8=2.000, -96.000, 0.000, 22.167, 1574.803, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 8.000, 0.000, 0.000 point.7=2.000, -100.083, 0.000, 2.683, 1574.803, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 9.000, 0.000, 0.000 static_pitch=0.0000000007 static_cg_height=17.55700 [GeneralEngineData] engine_type=1 Engine.0=-6.250, -13.950, -3.417 Engine.1=-8.333, -20.333, -4.833 Engine.2=-8.333, 20.333, -4.833 Engine.3=-6.250, 13.950, -3.417 fuel_flow_scalar=1.000 [TurbineEngineData] fuel_flow_gain=0.002 inlet_area=59.990 rated_N2_rpm=29920.000 static_thrust=49991.300 afterburner_available=1 reverser_available=1 [Reference Speeds] flaps_up_stall_speed=123.000 full_flaps_stall_speed=98.400 cruise_speed=1967.420 [keyboard_response] elevator=150.000, 250.000 aileron=150.000, 250.000 rudder=150.000, 250.000 [Views] eyepoint=83.495, 0.000, 7.395 [General] performance=Designer: Shigeru Tanaka\nModel file: sst2010.zip\nCopyright: Shigeru Tanaka\nProject: October 19, 2002\nEmail: wing.shigeru@nifty.ne.jp\nCopyright held lawfully by the auther under the international copyright law:\nDigital watermarking is the technology wherein copyright owner's identification information, copyright control information and the similar are embedded into digitally created data in such manner as not to be easily perceived, thereafter watermarking information is detected from the data at necessity, thereby copyright control and protection is duly conducted and effectively promoted.\nCopyright 2002 Shigeru Tanaka atc_type= atc_model= [autopilot] autopilot_available=1 flight_director_available=0 default_vertical_speed=1800.000 autothrottle_available=1 autothrottle_arming_required=1 autothrottle_takeoff_ga=1 autothrottle_max_rpm=90.000 pitch_takeoff_ga=8.000 [LIGHTS] //Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing light.0=3, -13, -27.06, -3.5, fx_navredh , light.1=3, -13, 27.06, -3.5, fx_navgreh , light.2=3, -101, 0.00, 5.3, fx_navwhih , light.3=2, 17, -4.5, -3.7, fx_navwhih , light.4=2, 17, 4.5, -3.7, fx_navwhih , light.5=2, -85, 0.00, 22, fx_strobeh , light.6=1, 30.05, 0.00, 5.8, fx_beaconh , light.7=1, -32.22, 0.00, -5.9, fx_beaconb , light.8=4, -16.24, 0.00, 9.19, fx_vclighth, [Radios] // Radio Type = availiable, standby frequency, has glide slope Audio.1 = 0 Com.1 = 1, 0 Com.2 = 1, 0 Nav.1 = 1, 0, 1 Nav.2 = 1, 0, 0 Adf.1 = 1 Transponder.1 = 1 Marker.1 = 1 [SMOKESYSTEM] smoke.0=-24.00,-70.00,20.00, fx_sst2010smoke smoke.1=-24.00,-65.00,14.00, fx_sst2010smoke smoke.2=2.00,-65.00,-14.00, fx_sst2010smoke smoke.3=3.00,-70.00,-20.00, fx_sst2010smoke smoke.4=-212.00,0,-150.00,20.00, fx_sst2010smoke_special smoke.5=-323.00,0,-145.00,14.00, fx_sst2010smoke_original smoke.6=178.00,0,-145.00,-14.00, fx_sst2010smoke_novel smoke.7=236.00,0,-150.00,-20.00, fx_sst2010smoke_innovative smoke.8=-128,-65.875,20.0000,fx_sst2010afterburner smoke.9=-229,-66.75,20.0000,fx_sst2010afterburner_special smoke.10=-330,-65.875,14.500,fx_sst2010afterburner smoke.11=-431,-66.75,14.500,fx_sst2010afterburner_original smoke.12=-532,-65.875,-14.500,fx_sst2010afterburner smoke.13=-633,-66.75,-14.500,fx_sst2010afterburner_novel smoke.14=-734,-65.875,-20.00,fx_sst2010afterburner smoke.15=-835,-66.650,-20.00,fx_sst2010afterburner_innovative smoke.100=0, 007, 0.007, -0.007, Marlboro Long Size [ALCHOLESYSTEM] brandy.0=0.07, 1048.71, 28.05, Courvoisier Cognac VSOP [EFFECTS] wake=fx_wake water=fx_spray dirt=fx_tchdrt concrete=fx_sparks touchdown=fx_tchdwn, 1 [direction_indicators] direction_indicator.0=3,0 [Flaps.0] type=1 span-outboard=0.500 extending-time=5.000 system_type=0 damaging-speed=0.000 blowout-speed=0.000 lift_scalar=1.000 drag_scalar=1.000 pitch_scalar=1.000 flaps-position.0=0.000, 0.000 flaps-position.1=4.999, 0.000 flaps-position.2=9.998, 0.000 flaps-position.3=14.997, 0.000 flaps-position.4=19.996, 0.000 flaps-position.5=24.995, 0.000 flaps-position.6=29.994, 0.000 flaps-position.7=34.993, 0.000 flaps-position.8=39.992, 0.000 [forcefeedback] gear_bump_nose_magnitude=3000 ; 0 - 10000 gear_bump_nose_direction=18000 ; 0 - 35999 degrees gear_bump_nose_duration=250000 ; in microseconds gear_bump_left_magnitude=2700 ; 0 - 10000 gear_bump_left_direction=35500 ; 0 - 35999 degrees gear_bump_left_duration=250000 ; in microseconds gear_bump_right_magnitude=2700 ; 0 - 10000 gear_bump_right_direction=00500 ; 0 - 35999 degrees gear_bump_right_duration=250000 ; in microseconds ground_bumps_magnitude1=1300 ; 0 - 10000 ground_bumps_angle1=08900 ; 0 - 35999 degrees ground_bumps_intercept1=3.0 ground_bumps_slope1=0.20 ground_bumps_magnitude2=200 ; 0 - 10000 ground_bumps_angle2=09100 ; 0 - 35999 degrees ground_bumps_intercept2=1.075 ground_bumps_slope2=0.035 crash_magnitude1=10000 ; 0 - 10000 crash_direction1=01000 ; 0 - 35999 degrees crash_magnitude2=10000 ; 0 - 10000 crash_direction2=9000 ; 0 - 35999 degrees crash_period2=75000 ; in microseconds crash_duration2=2500000 ; in microseconds