[fltsim.0] title=NASA Space Shuttle sim=shuttle model= panel= sound= texture= checklists= atc_id=OV102 atc_airline= atc_flight_number= ui_manufacturer=NASA ui_type=Space Shuttle ui_variation=Columbia description=This shuttle is the Orbit re-entry, descent and landing vehicle this remake of my original is dedicated to the brave astronauts who Tragicaly Lost their lives on mission STS-107 the crew are as follows: Crew: Commander Rick D. Husband, Pilot William C. McCool, Payload Specialist Michael P. Anderson, Mission Specialist Kalpana Chawla, Mission Specialist David M. Brown (first flight), Mission Specialist Laurel B. Clark, Payload Specialist Ilan Ramon, Israel may they all rest in piece. Enjoy this Space shuttle. atc_heavy=1 [General] atc_type=NASA atc_model=SHUTTLE editable=1 performance= [pitot_static] vertical_speed_time_constant=1 //Increasing this value will cause a more instantaneous reaction in the VSI max_number_of_stations=50 [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 [electrical] ;BusType, MaxAmpLoad, MinVoltage BusTypes:0=MainBus,1=AvionicsBus,2=BatteryBus,3=HotBatteryBus,4-7=Generator/AlternatorBus(1-4) flap_motor=0, 0 , 17.0 gear_motor=0, 0 , 17.0 autopilot=0, 0 , 17.0 avionics_bus=0, 10, 17.0 avionics=1, 0 , 17.0 pitot_heat=0, 0 , 17.0 additional_system=0, 0, 17.0 marker_beacon=1, 0 , 17.0 gear_warning=0, 0 , 17.0 fuel_pump=0, 0 , 17.0 starter1=0, 0, 17.0 light_nav=0, 0 , 17.0 light_beacon=0, 0 , 17.0 light_landing=0, 0 , 17.0 light_taxi=0, 0 , 17.0 light_strobe=0, 0 , 17.0 light_panel=0, 0 , 17.0 //0 Class <0=none,1=wheel, 2=scrape, 3=float> //1 Longitudinal Position (feet) //2 Lateral Position (feet) //3 Vertical Position (feet) //4 Impact Damage Threshold (Feet Per Minute) //5 Brake Map (0=None, 1=Left, 2=Right) //6 Wheel Radius (feet) //7 Steer Angle (degrees) //8 Static Compression (feet) (0 if rigid) //9 Max/Static Compression Ratio //10 Damping Ratio (0=Undamped, 1=Critically Damped) //11 Extension Time (seconds) //12 Retraction Time (seconds) //13 Sound Type //14 Airspeed limit for retraction (KIAS) //15 Airspeed that gear gets damage at (KIAS) [contact_points] //gear //nose gear point.0=1.000, 57.500, 0.000, -14.800, 1681.100, 0.000, 1.442, 55.920, 0.800, 2.500, 0.900, 4.000, 4.000, 0.000, 0.000, 0.000 //main left point.1=1.000, -9.600, -11.300, -18.800, 2574.800, 1.000, 1.442, 0.000, 1.000, 2.500, 0.900, 6.900, 6.900, 2.000, 0.000, 0.000 //main right point.2=1.000, -9.600, 11.300, -18.800, 2574.800, 2.000, 1.442, 0.000, 1.000, 2.500, 0.900, 7.100, 7.100, 3.000, 0.000, 0.000 //scrapes //left wing tip point.3=2.000, -28.700, -39.400, -5.300, 787.400, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 5.000, 0.000, 0.000 //right wing tip point.4=2.000, -28.700, 39.400, -5.300, 787.400, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 6.000, 0.000, 0.000 //tail point.5=2.000, -47.900, 0.000, -7.830, 787.400, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 9.000, 0.000, 0.000 //nose point.6=2.000, 70.100, 0.000, -4.100, 787.400, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 4.000, 0.000, 0.000 //nose upper point.7=2.000, 45.900, 0.000, 9.200, 787.400, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 4.000, 0.000, 0.000 //tail fin top point.8=2.000, -47.900, 0.000, 34.900, 787.400, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 4.000, 0.000, 0.000 //belly front left point.9=2.000, 47.800, -10.000, -9.600, 1000.400, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 4.000, 0.000, 0.000 //belly front right point.10=2.000, 47.800, 10.000, -9.600, 1000.400, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 4.000, 0.000, 0.000 //belly rear left point.11=2.000, -28.800, -10.000, -9.600, 1000.400, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 4.000, 0.000, 0.000 //belly rear right point.12=2.000, -28.800, 10.000, -9.600, 1000.400, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 4.000, 0.000, 0.000 max_number_of_points=21 static_pitch=-3.620 static_cg_height=14.660 [Views] eyepoint=48.155, -1.781, 6.265 //(feet) longitudinal, lateral, vertical distance from reference datum [Radios] // Radio Type=availiable, standby frequency, has glide slope Audio.1=1 Com.1=1, 1 Com.2=1, 1 Nav.1=1, 1, 1 Nav.2=1, 1, 0 Adf.1=1 Transponder.1=1 Marker.1=1 [keyboard_response] //Breakpoint speeds (knots) on the keyboard increments of control surfaces. //Speed at which the incremenet is reduced to 1/2 and 1/8 respectively. elevator=150, 250 aileron=150, 250 rudder=150, 250 [direction_indicators] //1 Type: 0=None, 1=Vacuum Gyro, 2=Electric Gyro, 3=Electro-Mag Slaved Compass, 4=Slaved to another //2 Indicator number of slaving indicator if Type=4 direction_indicator.0=3,0 [exits] number_of_exits=2 exit_rate.0=0.4 ;Percent per second exit_rate.1=0.4 ;Percent per second [EFFECTS] wake=fx_wake water=fx_spray dirt=fx_tchdrt concrete=fx_sparks touchdown=fx_tchdwn, 1 [SMOKESYSTEM] smoke.0=-67.0, 0, 7.8, fx_shuttle_exhaust smoke.1=-68.0, -5.7, -1, fx_shuttle_exhaust smoke.2=-68.0, 5.7, -1, fx_shuttle_exhaust [autopilot] autopilot_available=1 flight_director_available=1 default_vertical_speed=1800 autothrottle_available=1 autothrottle_arming_required=0 autothrottle_max_rpm=90 autothrottle_takeoff_ga=1 pitch_takeoff_ga=8; use_no_default_bank=1 use_no_default_pitch=1 [Reference Speeds] flaps_up_stall_speed=156.000 full_flaps_stall_speed=156.000 cruise_speed=500.000 [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 [GeneralEngineData] engine_type=1 Engine.0=-47.000, 0.000, 8.000 Engine.1=-48.600, -5.100, -0.700 Engine.2=-48.600, 5.100, -0.700 fuel_flow_scalar=1.000 [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=150000.000 empty_weight_roll_MOI=4500000.000 empty_weight_pitch_MOI=8000000.000 empty_weight_yaw_MOI=8500000.000 empty_weight_coupled_MOI=1300.000 max_gross_weight=176799.999 CG_forward_limit=0.000 CG_aft_limit=1.000 [fuel] LeftMain=0.000, 0.000, 0.000, 1000.000, 0.000 RightMain=0.000, 0.000, 0.000, 1000.000, 0.000 fuel_type=2.000000 number_of_tank_selectors=1 [airplane_geometry] wing_area=1389.000 wing_span=83.333 wing_root_chord=16.667 wing_dihedral=5.999 wing_incidence=0.000 wing_twist=-1.000 oswald_efficiency_factor=7.504 wing_winglets_flag=0 wing_sweep=0.000 wing_pos_apex_lon=0.000 wing_pos_apex_vert=0.000 htail_area=400.000 htail_span=50.000 htail_pos_lon=-62.500 htail_pos_vert=0.000 htail_incidence=0.000 htail_sweep=0.000 vtail_area=500.000 vtail_span=25.495 vtail_sweep=0.000 vtail_pos_lon=-60.833 vtail_pos_vert=5.833 elevator_area=100.000 aileron_area=55.560 rudder_area=85.000 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 [TurbineEngineData] fuel_flow_gain=0.002 inlet_area=120.242 rated_N2_rpm=29920.000 static_thrust=130000.000 afterburner_available=1 reverser_available=0
