[fltsim.0] title=victorbk1a sim=victor1 model=bk1a panel= sound= texture=57bk1 kb_checklists= ui_manufacturer=DSB Design ui_type=Handley Page Victor B.1A(K.2P) ui_variation=57 Sqdrn, 1976 description=The Victor B.1A(K.2P) was an interim conversion of the Victor B.1A to fill the 'tanker gap' caused by the premature retirement of the Vickers Valiant. This aircraft made its last flight in 1976, and today resides at the Imperial War Museum Duxford. © FSCAC 2003 [fltsim.1] title=victork1 sim=victor1 model=k1 panel= sound= texture=k1ttf kb_checklists= ui_manufacturer=DSB Design ui_type=Handley Page Victor K.1 ui_variation=TTF, 1968 description=Following the introduction of the Victor B.2 into service with Bomber Command, the redundant Victor B.1s were converted to tanker standard in order to replace the withdrawn Valiants. The Victor K.1 was the definitive mark one tanker conversion, this aircraft being operated by the Tanker Training Flight (TTF) circa 1968 [fltsim.2] title=victorb1a sim=victor1 model=b1a panel= sound= texture=57b1a kb_checklists= ui_manufacturer=DSB Design ui_type=Handley Page Victor B.1A ui_variation=57 Sqdrn, 1963 description=As an interim measure pending the introduction of the Victor B.2, the B.1s were upgraded through fitment of the 'Red Steer' tail warning radar, a refuelling probe and a new cockpit layout, among other enhancements. This aircraft was based at RAF Tengah in Singapore during 1963. [fltsim.3] title=victorb1awhite 15 sim=victor1 model=b1a panel= sound= texture=15b1a kb_checklists= ui_manufacturer=DSB Design ui_type=Handley Page Victor B.1A ui_variation=15 Sqdrn, 1962 description=As an interim measure pending the introduction of the Victor B.2, the B.1s were upgraded through fitment of the 'Red Steer' tail warning radar, a refuelling probe and a new cockpit layout, among other enhancements. This aircraft was based at RAF Cottesmore during 1962. [fltsim.4] title=victorb1awhite 55 sim=victor1 model=b1a panel= sound= texture=55b1a kb_checklists= ui_manufacturer=DSB Design ui_type=Handley Page Victor B.1A ui_variation=55 Sqdrn, 1962 description=As an interim measure pending the introduction of the Victor B.2, the B.1s were upgraded through fitment of the 'Red Steer' tail warning radar, a refuelling probe and a new cockpit layout, among other enhancements. This aircraft was based at RAF Honnington during 1962. [fltsim.5] title=victorb1 sim=victor1 model=b1 panel= sound= texture=10b1 kb_checklists= ui_manufacturer=DSB Design ui_type=Handley Page Victor B.1 ui_variation=10 Sqdrn, 1958 description=The Victor B.1 first entered service with No 10 Squadron in April 1958, becoming the last of the V-bombers to enter service. This aircraft was based at RAF Cottesmore during 1958. [electrical] ;BusType, MaxAmpLoad, MinVoltage BusTypes:0=MainBus,1=AvionicsBus,2=BatteryBus,3=HotBatteryBus,4-7=Generator/AlternatorBus(1-4) flap_motor=0, 5 , 17.0 gear_motor=0, 5 , 17.0 autopilot=0, 5 , 17.0 avionics_bus=0, 10, 17.0 avionics=1, 5 , 17.0 pitot_heat=0, 2 , 17.0 additional_system=0, 20, 17.0 marker_beacon=1, 2 , 17.0 gear_warning=0, 2 , 17.0 fuel_pump=0, 5 , 17.0 starter1=0, 20, 17.0 light_nav=0, 5 , 17.0 light_beacon=0, 5 , 17.0 light_landing=0, 5 , 17.0 light_taxi=0, 5 , 17.0 light_strobe=0, 5 , 17.0 light_panel=0, 5 , 17.0 [LIGHTS] //Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit light.0 = 3, -18.0, -53.0, -4.0, fx_navred , light.1 = 3, -18.0, 53.0, -4.0, fx_navgre , light.2 = 1, 25, 0.00, 2.6, fx_beaconh , light.4 = 3, -50.5, 1.5, 7.8, fx_navwhi , light.5 = 3, -50.5, -1.5, 7.8, fx_navwhi , light.6 = 3, -5.6, 18.7, -4.5, fx_navwhi , light.7 = 3, -5.6, -20, -4.5, fx_navwhi , [WEIGHT_AND_BALANCE] reference_datum_position=0.000000,0.000000,0.000000 empty_weight_CG_position=0.000000,0.000000,0.000000 CG_forward_limit=0.000000 CG_aft_limit=1.000000 max_number_of_stations=50 station_load.0=0.000000,0.000000,0.000000,0.000000 empty_weight=79000.000000 empty_weight_roll_MOI=2850000.000000 empty_weight_pitch_MOI=5650000.000000 empty_weight_yaw_MOI=3780000.000000 empty_weight_coupled_MOI=1600.000000 max_gross_weight=185000.000000 [forcefeedback] gear_bump_nose_magnitude=6000 gear_bump_nose_direction=18000 gear_bump_nose_duration=250000 gear_bump_left_magnitude=6000 gear_bump_left_direction=35500 gear_bump_left_duration=250000 gear_bump_right_magnitude=6000 gear_bump_right_direction=00500 gear_bump_right_duration=250000 ground_bumps_magnitude1=1500 ground_bumps_angle1=8900 ground_bumps_intercept1=5.0 ground_bumps_slope1=0.48 ground_bumps_magnitude2=750 ground_bumps_angle2=9100 ground_bumps_intercept2=0.075 ground_bumps_slope2=1.0 crash_magnitude1=10000 crash_direction1=01000 crash_magnitude2=10000 crash_direction2=9000 crash_period2=75000 crash_duration2=2500000 [SMOKESYSTEM] smoke.0=0.00,-6.00,-7.30, PSS_smokeyvl smoke.1=0.00,-6.00,-10.50, PSS_smokeyvl smoke.2=0.00,-6.00,10.50, PSS_smokeyvl smoke.3=0.00,-6.00,7.30, PSS_smokeyvl [Views] eyepoint=31.5,-1.5,1.5 [keyboard_response] elevator=0.000000,0.000000 aileron=0.000000,0.000000 rudder=0.000000,0.000000 [direction_indicators] direction_indicator.0=3,0 [jet_engine] thrust_scalar=1.000 [flight_tuning] cruise_lift_scalar=1.100 pitch_stability=1.000 roll_stability=2.000 yaw_stability=1.000 parasite_drag_scalar=0.8 induced_drag_scalar=0.8 elevator_effectiveness=1.000 aileron_effectiveness=1.000 rudder_effectiveness=1.000 [contact_points] point.0=1.000000,27.666667,0.000000,-10.50000,1574.803200,0.000000,1.440955,30.920000,0.5147,2.500000,1.197584,4.000000,4.000000,0.000000,0.000000,0.000000 point.1=1.000000,-5.583333,-17.00,-10.0000,1574.803200,1.000000,1.440955,2.000000,0.711378,2.500000,0.640653,6.000000,6.000000,2.000000,0.000000,0.000000 point.2=1.000000,-5.583333,17.0,-10.0000,1574.803200,2.000000,1.440955,2.000000,0.711378,2.500000,0.640653,6.000000,6.000000,3.000000,0.000000,0.000000 point.3=2.000000,-0.333333,-50.416667,2.916667,1574.803200,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,5.000000,0.000000,0.000000 point.4=2.000000,-0.333333,50.416667,2.916667,1574.803200,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,6.000000,0.000000,0.000000 point.5=2.000000,-53.000000,0.000000,-4.000000,1574.803200,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,9.000000,0.000000,0.000000 point.6=2.000000,36.000000,0.000000,2.416667,1574.803200,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,4.000000,0.000000,0.000000 //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) static_pitch=0.000000 static_cg_height=10.293726 gear_system_type=1 [General] performance=Model : Chris Hodgson\nPanel: Aled Hughes\nFlight model : Chris Hodgson [fuel] Center1=0.000000,0.000000,0.000000,4000.000000,3.000000 LeftMain=0.000000,-9.065000,-0.920000,4600.500000,0.000000 RightMain=0.000000,9.065000,-0.920000,4000.500000,0.000000 fuel_type=2.000000 number_of_tank_selectors=1 electric_pump=0 [airplane_geometry] wing_area=2406.000000 wing_span=110.000000 wing_root_chord=24.666667 wing_dihedral=2.499390 wing_incidence=1.378784 wing_twist=1.400757 oswald_efficiency_factor=0.911509 wing_winglets_flag=65280 wing_sweep=-20 wing_pos_apex_lon=-2.588926 wing_pos_apex_vert=0.000000 htail_area=337.000000 htail_span=40.833333 htail_pos_lon=-33.333333 htail_pos_vert=0.000000 htail_incidence=0.000000 htail_sweep=0.000000 vtail_area=138.000000 vtail_span=13.394029 vtail_sweep=30.000000 vtail_pos_lon=-33.333333 vtail_pos_vert=3.333333 elevator_area=39.500000 aileron_area=18.000000 rudder_area=21.960000 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 [Flaps.0] type=1 span-outboard=0.500000 extending-time=5.000000 system_type=0 flaps-position.0=0.000000,0.000000 flaps-position.1=13.330818,0.000000 flaps-position.2=39.992454,0.000000 [GeneralEngineData] engine_type=1 Engine.0=0.000000,-10.000000,0.000000 Engine.1=0.000000,-6.666667,0.000000 Engine.2=0.000000,6.666667,0.000000 Engine.3=0.000000,10.000000,0.000000 fuel_flow_scalar=1.000000 min_throttle_limit=-0.249939 [TurbineEngineData] fuel_flow_gain=0.011000 inlet_area=1.000000 rated_N2_rpm=29920.000000 static_thrust=11050.000000 afterburner_available=0 reverser_available=0 [Reference Speeds] flaps_up_stall_speed=180.000000 full_flaps_stall_speed=120.000000 cruise_speed=480.317157 max_indicated_speed=665.000000 max_mach=0.95 [autopilot] autopilot_available=1 flight_director_available=0 default_vertical_speed=1800.000000 autothrottle_available=1 autothrottle_arming_required=0 autothrottle_takeoff_ga=0 autothrottle_max_rpm=90.000000 pitch_takeoff_ga=8.000000 max_pitch=10.000000 max_pitch_acceleration=1.000000 max_pitch_velocity_lo_alt=2.000000 max_pitch_velocity_hi_alt=1.500000 max_pitch_velocity_lo_alt_breakpoint=20000.000000 max_pitch_velocity_hi_alt_breakpoint=28000.000000 max_bank=25.000000 max_bank_acceleration=1.800000 max_bank_velocity=3.000000 max_throttle_rate=0.100000 nav_proportional_control=9.000000 nav_integrator_control=0.250000 nav_derivative_control=0.000000 nav_integrator_boundary=2.500000 nav_derivative_boundary=0.000000 gs_proportional_control=9.520000 gs_integrator_control=0.260000 gs_derivative_control=0.000000 gs_integrator_boundary=0.700000 gs_derivative_boundary=0.000000 yaw_damper_gain=0.000000 [brakes] toe_brakes_scale=1.000031 parking_brake=1 [gear_warning_system] gear_warning_available=0 pct_throttle_limit=0.000000 flap_limit_power=0.000000 flap_limit_idle=0.000000 [hydraulic_system] electric_pumps=0 engine_map=1,1,1,1 normal_pressure=3000.000000 [stall_warning] type=1 [attitude_indicators] attitude_indicator.0=1 [turn_indicators] turn_indicator.0=1,0 [TailHook] tailhook_length=1 ;(feet) tailhook_position=-15.0, 0.0, -1.0 ;(feet) longitudinal, lateral, vertical positions from datum cable_force_adjust=0 [folding_wings] wing_fold_system_type = 4 fold_rates = 0.20 [EFFECTS] wake=fx_wake water=fx_spray dirt=fx_tchdrt concrete=fx_sparks touchdown=fx_tchdwn, 1