[fltsim.0] title=Vampire MkI Aussie sim=VampAus_MKI model=VampAus_MKI [General] editable=0 [WEIGHT_AND_BALANCE] max_gross_weight =10480.000000 empty_weight =6372.000000 reference_datum_position =10.000000,0.000000,0.000000 empty_weight_CG_position =-11.200000,0.000000,0.000000 max_number_of_stations = 50 station_load.0 =170.000000,-6.000000,0.000000,0.000000 ;Moments of Inertia empty_weight_pitch_MOI =8057.000000 empty_weight_roll_MOI =7418.000000 empty_weight_yaw_MOI =15543.000000 empty_weight_coupled_MOI =0.000000 CG_forward_limit=0.000000 CG_aft_limit=1.000000 [fuel] Center1 =-8.000000,0.000000,0.000000,178.000000,0.000000 LeftMain =-5.000000,-2.800000,0.000000,26.000000,0.000000 RightMain =-5.000000,2.800000,0.000000,26.000000,0.000000 fuel_type = 2 //Fuel type: 1 = Avgas, 2 = JetA number_of_tank_selectors = 1 [airplane_geometry] wing_area =266.000000 wing_span =40.000000 wing_root_chord =9.300000 wing_dihedral =3.000000 wing_incidence =0.500000 wing_twist =0.000000 oswald_efficiency_factor=0.770000 wing_winglets_flag =0 wing_sweep =12.000000 wing_pos_apex_lon =-7.000000 wing_pos_apex_vert =0.000000 htail_area =33.200000 htail_span =8.900000 htail_pos_lon =-25.900000 htail_pos_vert =3.500000 htail_incidence =-0.500000 htail_sweep =0.000000 vtail_area =14.400000 vtail_span =5.500000 vtail_sweep =33.000000 vtail_pos_lon =-25.700000 vtail_pos_vert =0.700000 elevator_area =10.800000 aileron_area =12.600000 rudder_area =9.000000 elevator_up_limit =20.000000 elevator_down_limit =20.000000 aileron_up_limit =16.000000 aileron_down_limit =16.000000 rudder_limit =25.000000 elevator_trim_limit =15.000000 spoiler_limit =90.000000 spoilerons_available =0 aileron_to_spoileron_gain =4.600000 min_ailerons_for_spoilerons =5.000000 min_flaps_for_spoilerons=0.000000 [Flaps.0] type=1 span-outboard=0.500000 extending-time=4.000000 system_type=1 damaging-speed=160.000000 blowout-speed=190.000000 lift_scalar=1.000000 drag_scalar=1.000000 pitch_scalar=1.000000 flaps-position.0=0.000000 flaps-position.1=20.000000 flaps-position.2=40.000000 flaps-position.3=80.000000 [Reference Speeds] flaps_up_stall_speed =83.0 full_flaps_stall_speed =75.0 cruise_speed =300.0 [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 [contact_points] //0 Class //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) point.0=1.000000,-1.600000,0.000000,-4.20000,1181.100000,0.000000,0.700000,60.000000,0.3,2.50000,0.587800,10.000000,10.000000,0.000000,175.000000,185.000000 point.1=1.000000,-12.400000,-6.100000,-3.000000,1574.800000,1.000000,1.050000,0.000000,0.479800,2.500000,0.745600,9.000000,9.000000,2.000000,175.000000,185.000000 point.2=1.000000,-12.400000,6.100000,-3.000000,1574.800000,2.000000,1.050000,0.000000,0.479800,2.500000,0.745600,7.000000,7.000000,3.000000,175.000000,185.000000 point.3=2.000000,0.000000,0.000000,0.000000,2100.00000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,9.000000,0.000000,0.000000 point.4=2.000000,-7.000000,0.000000,-1.300000,3000.00000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,4.000000,0.000000,0.000000 point.5=2.000000,-13.700000,-20.000000,2.100000,787.400000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,5.000000,0.000000,0.000000 point.6=2.000000,-13.700000,20.000000,2.100000,787.400000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,6.000000,0.000000,0.000000 point.7=2.000000,-30.000000,-4.900000,5.800000,787.400000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,9.000000,0.000000,0.000000 point.8=2.000000,-30.000000,4.900000,5.800000,787.400000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,9.000000,0.000000,0.000000 point.9=2.000000,-30.000000,4.900000,2.000000,1200.00000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,9.000000,0.000000,0.000000 point.10=2.000000,-30.000000,-4.900000,2.000000,1200.00000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,9.000000,0.000000,0.000000 point.11=2.000000,-13.700000,-10.000000,2.100000,1000.00000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,5.000000,0.000000,0.000000 point.12=2.000000,-13.700000,10.000000,2.100000,1000.00000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,6.000000,0.000000,0.000000 static_pitch =6.0 static_cg_height =2.74 [GeneralEngineData] engine_type =1 Engine.0 =-12.4,0.0,0.0 [TurbineEngineData] fuel_flow_gain =0.0025 inlet_area =1.75 rated_N2_rpm =10000.0 static_thrust =3100.0 afterburner_available =0 reverser_available =0 fuel_flow_scalar=1.0 thrust_scalar=1.0 [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 [forcefeedback] stick_shaker_magnitude=5000 ; 0 - 10000 stick_shaker_direction=0 ; 0 - 35999 degrees stick_shaker_period=111111 ; in microseconds 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=9000 ; 0 - 35999 degrees gear_bump_left_duration=250000 ; in microseconds gear_bump_right_magnitude=2700 ; 0 - 10000 gear_bump_right_direction=27000 ; 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