//FS9 Version 2.0 3:46 PM 1/13/2004 [fltsim.0] title=ALPHA Su-47 Berkut sim=Berkut model= panel= sound= texture= atc_id=SU47 kb_checklists=Berkut_check kb_reference=Berkut_ref ui_manufacturer=ALPHA ui_type=Sukhoi Su-47 'Berkut' ui_variation=Technology demonstrator description=© ALPHA Simulations 2004\n\nSukhoi Su-47 'Berkut'\n\nThe Su-47 (or S-37) is an experimental fighter technology demonstrator built to validate and gain experience with various technology advances (particularly the forward swept wings) which could be incorporated into a fifth generation Sukhoi fighter. The 'Berkut' or 'Golden Eagle' has extremely high agility at subsonic speeds enabling the aircraft to alter its angle of attack and its flight path very quickly, and it also retains manoeuvrability in supersonic flight. It first flew in September 1997 and completed the first stage of flight trials in December 2001. atc_id_color=0000000000 visual_damage=0 [General] atc_type=EXPERIMENTAL performance=Model Designer : P McDonell / P Perrott\nPanel : P Perrott\nFlight model : J McDaniel\n\nType: Fighter technology demonstrator\nWing Span: 16.7m (54.7ft) \nLength: 22.6m (74ft) \nHeight: 6.4m (21 ft) \nWeight: Normal takeoff 25,670kg (56,590lb) \nWeight: max takeoff 34,000kg (74,690lb) \nMax. speed at 30,000ft: 2200km/h (1188kt)\nMax. speed at sea level: 1400km/h (756m/h)\nService ceiling: 59,000ft\nBasic range: 3300km (1 782nm)\nPower Plant: Two 152kN (34,200lb) with afterburning Aviadvigatel D-30F6 turbofans. May later be fitted with two 196kN (44,000lb) with afterburning and thrust-vectoring Saturn AL-31 F turbofans.\nArmament: None in the prototype. A production version would carry air-to-air and air-to-ground weapons in internal weapons bays and on external pylons.\nOperators: Experimental aircraft, not in operational service.\n editable=0 Category=airplane [weight_and_balance] // ACM V2.3 max_gross_weight = 74957 empty_weight = 45216 reference_datum_position = 0, 0, 0 empty_weight_CG_position = 0, 0, 0 empty_weight_pitch_MOI = 21030 empty_weight_roll_MOI = 45075 empty_weight_yaw_MOI = 65720 empty_weight_coupled_MOI = 0 max_number_of_stations = 1 station_load.0 = 200, 19.42, 0.0, 1.70 [lights] //Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing light.0 = 2, 7.70, -27.00, 0.00, fx_Vortices light.1 = 2, 7.70, 27.00, 0.00, fx_Vortices light.2 = 3, 7.90, -28.00, 0.25, fx_navred light.3 = 3, 7.90, 28.00, 0.25, fx_navgre light.4 = 3, -21.25, -9.80, 9.30, fx_navwhi light.5 = 3, -21.25, 9.80, 9.30, fx_navwhi light.6 = 4, 29.00, 0.00, 2.50, fx_vclight //light.7 = 9, -28, -2.30, 0.2, sr_burner_Port //light.8 = 9, -28, 2.30, 0.2, sr_burner_Starboard light.15= 6, -18.0, -2.3, 0.0, fx_Bob_burn_blue light.16= 6, -18.0, 2.3, 0.0, fx_Bob_burn_blue light.17= 6, -23.5, -2.3, -0.8, fx_F14_Burnerflame light.18= 6, -23.5, 2.3, -0.8, fx_F14_Burnerflame [GeneralEngineData] //0=Piston, 1=Jet, 2=None, 3=Helo-Turbine, 4=Rocket, 5=Turboprop engine_type = 1 fuel_flow_scalar = 0.70 engine.0 = -20, 2.3, 0, engine.1 = -20, -2.3, 0, min_throttle_limit=0.00 [TurbineEngineData] fuel_flow_gain=0.002 inlet_area=28.5 rated_N2_rpm=29920.00 static_thrust=34000.00 afterburner_available=3 reverser_available=0 [smokesystem] smoke.0 = 0, -80, -2.30, fx_eng_exhaust_gry smoke.1 = 0, -80, 2.30, fx_eng_exhaust_gry [effects] wake = fx_wake water = fx_spray dirt = fx_tchdrt concrete = fx_sparks touchdown = fx_tiremark_6 contrail = fx_contrail_l [fuel] //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons) Center1 = 0, 0, 0, 2500, 0 fuel_type = 2 number_of_tank_selectors = 1 electric_pump=0 [contact_points] static_pitch = 1.94 static_cg_height = 7.35 max_number_of_points = 17 point.0 = 1, 25.8,-0.60, -8.325, 2000, 0, 0.9, 45, 0.12, 3.2, 0.875, 5, 5, 0, 260, 325 point.1 = 1, 25.8, 0.60, -8.325, 2000, 0, 0.9, 45, 0.12, 3.2, 0.875, 5, 5, 0, 260, 325 point.2 = 1, -1.2, -6, -7.8, 2000, 1, 1.65, 0, 0.5, 2.5, 0.786, 5, 5, 2, 260, 325 point.3 = 1, -1.2, 6, -7.8, 2000, 2, 1.65, 0, 0.5, 2.5, 0.786, 5, 5, 3, 260, 325 point.4 = 2, 7.70, -27.80, 0.30, 1574.80, 0, 0, 0, 0, 0, 0, 0, 0, 5, 0, 0 point.5 = 2, 7.70, 27.80, 0.30, 1574.803, 0, 0, 0, 0, 0, 0, 0, 0, 6, 0, 0 point.6 = 2, -22.50, -2.50, -1.40, 1574.803, 0, 0, 0, 0, 0, 0, 0, 0, 9, 0, 0 point.7 = 2, -22.50, 2.50, -1.40, 1574.803, 0, 0, 0, 0, 0, 0, 0, 0, 9, 0, 0 point.8 = 2, 44.50, 0, -1.80, 1574.803, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0 gear_system_type=1 [keyboard_response] elevator = 150.00, 250.00 aileron = 150.00, 150.00 rudder = 150.00, 250.00 [forcefeedback] gear_bump_nose_magnitude = 1000 gear_bump_nose_direction = 18000 gear_bump_nose_duration = 250000 gear_bump_left_magnitude = 2000 gear_bump_left_direction = 35500 gear_bump_left_duration = 250000 gear_bump_right_magnitude = 2000 gear_bump_right_direction = 500 gear_bump_right_duration = 250000 ground_bumps_magnitude1 = 1250 ground_bumps_angle1 = 8900 ground_bumps_intercept1 = 5 ground_bumps_slope1 = 0.48 ground_bumps_magnitude2 = 450 ground_bumps_angle2 = 9100 ground_bumps_intercept2 = 0.075 ground_bumps_slope2 = 1 crash_magnitude1 = 2000 crash_direction1 = 1000 crash_magnitude2 = 2000 crash_direction2 = 9000 crash_period2 = 7500 crash_duration2 = 2500000 stick_shaker_magnitude = 2000 stick_shaker_direction = 0 stick_shaker_period = 111111 [airplane_geometry] wing_area = 600 wing_span = 55.74 wing_root_chord = 13.00 wing_dihedral = -3.0 wing_incidence = 0 wing_twist = 0 oswald_efficiency_factor = 0.925 wing_winglets_flag = 0 wing_sweep = -23 wing_pos_apex_lon = 3.00 wing_pos_apex_vert = 0.30 htail_area = 24.00 htail_span = 22.29 htail_pos_lon = 18.80 htail_pos_vert = 0.50 htail_incidence = 0.00 htail_sweep = 46 vtail_area = 102 vtail_span = 8.89 vtail_sweep = 46 vtail_pos_lon = -7.50 vtail_pos_vert = 1.00 elevator_area = 64 aileron_area = 47.5 rudder_area = 51 elevator_up_limit = 18 elevator_down_limit = 12 aileron_up_limit = 20 aileron_down_limit = 15 rudder_limit = 22 elevator_trim_limit = 19 spoiler_limit = 0 aileron_to_spoileron_gain = 0 min_ailerons_for_spoilerons = 0 min_flaps_for_spoilerons = 0 spoilerons_available = 0 auto_spoiler_available=0 positive_g_limit_flaps_up=14.00 positive_g_limit_flaps_down=10.00 negative_g_limit_flaps_up=-8.00 negative_g_limit_flaps_down=-7.00 [electrical] max_battery_voltage = 24 generator_alternator_voltage = 28 max_generator_alternator_amps = 155 electric_always_available = 0 [exits] number_of_exits=1 exit_rate.0=1.0 ;Percent per second [Views] eyepoint=28.0,0.0,3.25 [autopilot] autopilot_available=1 flight_director_available=1 default_vertical_speed=2000.00 autothrottle_available=1 autothrottle_arming_required=0 autothrottle_takeoff_ga=0 autothrottle_max_rpm=100.00 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 editable=0 [Flaps.0] type= 1 span-outboard= 0.5 extending-time= 5.00 system_type= 0 damaging-speed= 300.00 blowout-speed= 350.00 lift_scalar= 1.00 drag_scalar= 1.00 pitch_scalar= 1.00 flaps-position.0= 0.00, 0.00 flaps-position.1= 22.00, 300.00 flaps-position.2= 45.00, 270.00 flaps-position.3= 67.00, 240.00 flaps-position.4= 90.00, 225.00 [Flaps.1] type= 2 span-outboard= 0.5 extending-time= 2.00 system_type= 0 damaging-speed= 300.00 blowout-speed= 350.00 lift_scalar= 1.00 drag_scalar= 1.00 pitch_scalar= 1.00 flaps-position.0=0 flaps-position.1=0.25 flaps-position.2=0.5 flaps-position.3=0.75 flaps-position.4=1.0 [Reference Speeds] flaps_up_stall_speed=119 full_flaps_stall_speed=95 cruise_speed=mach 1.48 //500 knots indciated at 38,000 ft. max_indicated_speed=1350.00 max_mach=2.20 max_level_speed=mach 1.95 //at 30,000 ft. [brakes] toe_brakes_scale=1.08 parking_brake=1 [gear_warning_system] gear_warning_available=1 pct_throttle_limit=0.1 flap_limit_power=25 flap_limit_idle=5 [hydraulic_system] electric_pumps=0 engine_map=1,1,0,0 normal_pressure=3000.00 [stall_warning] type=1 stick_shaker=1 [attitude_indicators] attitude_indicator.0=1 [turn_indicators] turn_indicator.0=1,0 [pitot_static] pitot_heat=1.00 [vacuum_system] max_pressure=5.15 vacuum_type=2 electric_backup_pressure=0.00 engine_map=0,0,0,0 [pneumatic_system] max_pressure=18.00 bleed_air_scalar=1.00 [deice_system] structural_deice_type=0