//Alphasim FS2002 RF-4C Phantom II Version 1 [fltsim.0] title=ALPHA RF-4C Phantom II sim=RF-4C model= panel=f15 sound= texture= KB_checklists=F4_check kb_reference=F4_ref ui_manufacturer=McDonnell_Douglas ui_type=RF-4C Phantom II ui_variation=Hill Grey II scheme description=© ALPHA Simulations 2002\n\nMcDonnell Douglas RF-4C Phantom II\n\nIntended as a replacement for the RF-101C, this unarmed tactical recon version soon became the standard USAF aircraft in this category. Fitted with an array of optical, radar and IR sensors and with a combat range of 1000 miles, the new RF-4C was an ideal candidate for the role. The first flight was in May 1964. The 503rd and last example was delivered in 1973. In later years, RF-4Cs were armed with AIM-9 missiles for self-defense.\n\n\n\n [General] performance=Model Designer : Michael Davies\nTextures : Frank Safranek\nPanel : Phil Perrott\nFlight model & DP : Larry Vrooman\n\nMax Speed:\t 1,459 mph (Mach 2.25)\nCruise Speed:\t 587 kts\nInitial Rate of Climb: 28,000 fpm\nMaximum Range:\t 2,300 miles \nService Ceiling: 59,400 ft\nEmpty Weight:\t 28,276 lbs\nCombat Weight: 39,773\nMax TO Weight:\t 58,000 lbs\nEngine: (2) J-79-GE-15 turbojet, 17,900 lb st with AB. [SMOKESYSTEM] smoke.0=-3.50,-12.00,-2.50, fx_smoke_f6 smoke.1=-3.50,-12.00, 2.50, fx_smoke_f6 [WEIGHT_AND_BALANCE] empty_weight=28276 // (pounds) reference_datum_position=0.0, 0, 0 // (feet) distance from FlightSim Reference position: (1/4 chord, centerline, waterline) empty_weight_CG_position=0.0, 0, 0 // (feet) longitudinal, lateral, vertical distance from specified datum max_number_of_stations=50 station_load.0=210, 18.0, 0.0, 3.5 //Pilot Weight (lbs), longitudinal, lateral, vertical positions from datum (feet) station_load.0=210, 16.0, 0.0, 3.7 ;Moments of Inertia empty_weight_pitch_MOI=162663.00 empty_weight_roll_MOI=222777.00 empty_weight_yaw_MOI=582902.00 empty_weight_coupled_MOI=0.00 max_gross_weight=48094.00 [TailHook] tailhook_length=8 ;(feet) tailhook_position=-18.85, 0.0, -1.3 ;(feet) longitudinal, lateral, vertical positions from datum cable_force_adjust=1.0 [LSO] LSOAdjustSpeed=0.6 [exits] number_of_exits=1 exit_rate.0=1.0 ;Percent per second [ELECTRICAL] max_battery_voltage=24.0 generator_alternator_voltage=28.0 max_generator_alternator_amps=50.0 ;BusType, MaxAmpLoad, MinVoltage BusTypes:0=MainBus,1=AvionicsBus,2=BatteryBus,3=HotBatteryBus,4-7=Generator/AlternatorBus(1-4) flap_motor=0, 5 , 0.0 gear_motor=0, 5 , 0.0 autopilot=0, 5 , 0.0 avionics_bus=0, 10, 0.0 avionics=1, 5 , 0.0 pitot_heat=0, 2 , 0.0 additional_system=0, 20, 0.0 marker_beacon=1, 2 , 0.0 gear_warning=0, 2 , 0.0 fuel_pump=0, 5 , 0.0 starter1=0, 20, 0.0 light_nav=0, 5 , 0.0 light_beacon=0, 5 , 0.0 light_landing=0, 5 , 0.0 light_taxi=0, 5 , 0.0 light_strobe=0, 5 , 0.0 light_panel=0, 5 , 0.0 [flaps.0] type=1 // 1 - tail, 2 - lead span-outboard=0.125 // 0.0 .. 1.0 extending-time=5 // seconds flaps-position.0=0 // degrees, KIAS flaps-position.1=16 // degrees, KIAS flaps-position.2=32 // degrees, KIAS flaps-position.3=48 // degrees, KIAS flaps-position.4=80 // degrees, KIAS damaging-speed=350 // KIAS blowout-speed=500 // KIAS [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=3250 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 [contact_points] point.0=1,21.80,-0.50,-5.50,1574.80,0,0.70,43.80,0.20,2.50,0.95,6.00,6.00,0.00,0.00,0.00 point.1=1,21.80,0.50,-5.50,1574.80,0,0.70,43.80,0.20,2.50,0.95,6.00,6.00,0.00,0.00,0.00 point.2=1,-2.50,-9.60,-5.58,1574.80,1,1.30,0.00,0.230,2.50,0.950,5.00,5.00,2.00,0.00,0.00 point.3=1,-2.50,9.60,-5.58,1574.80,2,1.30,0.00,0.230,2.50,0.950,5.00,5.00,3.00,0.00,0.00 point.4=2,-13.30,-20.67,0.97,1574.80,0.00,0.00,0.00,0.00,0.00,0.00,0.00,0.00,5.00,0.00,0.00 point.5=2,-13.30,20.67,0.97,1574.80,0.00,0.00,0.00,0.00,0.00,0.00,0.00,0.00,6.00,0.00,0.00 point.6=2,-28.00,0.00,3.80,1574.80,0.00,0.00,0.00,0.00,0.00,0.00,0.00,0.00,9.00,0.00,0.00 point.7=2,29.20,0.00,-0.90,1574.80,0.00,0.00,0.00,0.00,0.00,0.00,0.00,0.00,4.00,0.00,0.00 static_pitch=-0.499878 static_cg_height=5.415919 gear_system_type=0 [Views] eyepoint=18.70,0.0,4.5 [fuel] Center1= 0.00, 0.00, 0.00, 1140.00, 0.00 LeftMain= 0.00,-1.50, -0.20, 630.00, 0.00 RightMain=0.00, 1.50, -0.20, 630.00, 0.00 External1=0.00, 0.00, -0.50, 280.00, 0.00 External2=0.00, 0.00, -0.50, 280.00, 0.00 fuel_type=2 number_of_tank_selectors=1 electric_pump=0 [airplane_geometry] wing_area=530.00 wing_span=38.33 wing_root_chord=19.90 wing_dihedral=2.499390 wing_incidence=0.00 wing_twist=0.00 oswald_efficiency_factor=0.659254 wing_winglets_flag=0 wing_sweep=50.00 wing_pos_apex_lon=10.40 wing_pos_apex_vert=0.00 htail_area=186.00 htail_span=18.0 htail_pos_lon=-19.60 htail_pos_vert=3.70 htail_incidence=-0.988770 htail_sweep=50.00 vtail_area=246.00 vtail_span=5.50 vtail_sweep=60.00 vtail_pos_lon=-12.30 vtail_pos_vert=5.80 elevator_area=56.390 aileron_area=19.940 rudder_area=15.040 elevator_up_limit=26.000825 elevator_down_limit=26.000825 aileron_up_limit=31.718944 aileron_down_limit=12.811336 rudder_limit=30.000070 elevator_trim_limit=25.783101 spoiler_limit=59.988681 spoilerons_available=0 aileron_to_spoileron_gain=0.00 min_ailerons_for_spoilerons=0.00 min_flaps_for_spoilerons=0.00 [GeneralEngineData] engine_type=1 Engine.0=-12.00,-2.40, 0.20 Engine.1=-12.00, 2.40, 0.20 fuel_flow_scalar=0.60 min_throttle_limit=0.00 [TurbineEngineData] fuel_flow_gain=0.001500 inlet_area=12.90 rated_N2_rpm=29920.00 static_thrust=17900.00 afterburner_available=1 reverser_available=0 [Reference Speeds] flaps_up_stall_speed=125.00 full_flaps_stall_speed=100.00 cruise_speed=712.00 max_indicated_speed=1600.00 max_mach=2.50 max_level_speed=mach 2.25 [keyboard_response] elevator=150.00,250.00 aileron= 150.00,250.00 rudder= 150.00,250.00 [autopilot] autopilot_available=1 flight_director_available=1 default_vertical_speed=1800.00 autothrottle_available=1 autothrottle_arming_required=0 autothrottle_takeoff_ga=0 autothrottle_max_rpm=125.00 pitch_takeoff_ga=8.00 max_pitch=10.00 max_pitch_acceleration=1.00 max_pitch_velocity_lo_alt=2.00 max_pitch_velocity_hi_alt=1.50 max_pitch_velocity_lo_alt_breakpoint=20000.00 max_pitch_velocity_hi_alt_breakpoint=28000.00 max_bank=25.00 max_bank_acceleration=1.80 max_bank_velocity=3.00 max_throttle_rate=0.10 nav_proportional_control=9.00 nav_integrator_control=0.250 nav_derivative_control=0.00 nav_integrator_boundary=2.50 nav_derivative_boundary=0.00 gs_proportional_control=9.520 gs_integrator_control=0.260 gs_derivative_control=0.00 gs_integrator_boundary=0.70 gs_derivative_boundary=0.00 yaw_damper_gain=0.00 [direction_indicators] direction_indicator.0=3,0 [LIGHTS] //Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing light.0=3, -9.76, -20.76, 0.97, fx_navred, // wing (red) light.1=3, -9.76, 20.76, 0.97, fx_navgre, // wing (green) light.2=1, -27.10, 0.00, 11.40, fx_beaconh, // tail beacon light.3=3, -13.50, -20.70, 0.97, fx_navwhi, // wing (white) light.4=3, -13.50, 20.70, 0.97, fx_navwhi, // wing (white) //afterburner effects light.11= 6, -13.7, -2.4, -0.20, fx_F14_Burn1 , // Eng1 Afterburner Burn1 light.12= 6, -13.7, -2.4, -0.20, fx_F14_Burn2 , // Eng1 Afterburner Burn2 light.13= 6, -16.3, -2.4, -0.30, fx_F14_Burnerflame , // Eng1 Afterburner Flame light.14= 7, -13.7, 2.4, -0.20, fx_F14_Burn1 , // Eng2 Afterburner Burn1 light.15= 7, -13.7, 2.4, -0.20, fx_F14_Burn2 , // Eng2 Afterburner Burn2 light.16= 7, -16.3, 2.4, -0.30, fx_F14_Burnerflame , // Eng2 Afterburner Flame light.17= 6, -13.0, -2.4, 0.10, fx_F14_Blueflame , // Eng1 Blueflame, light.18= 7, -13.0, 2.4, 0.10, fx_F14_Blueflame , // Eng2 Blueflame, [brakes] toe_brakes_scale=1.0031 parking_brake=1 [gear_warning_system] gear_warning_available=1 pct_throttle_limit=0.099976 flap_limit_power=25.496622 flap_limit_idle=5.042029 [hydraulic_system] electric_pumps=0 engine_map=1,1,0,0 normal_pressure=3000.00 [stall_warning] type=1 [attitude_indicators] attitude_indicator.0=1 [turn_indicators] turn_indicator.0=1,0
