[fltsim.0] title=Dart Kitten II sim=DartKitten model= panel= sound= texture= checklists= kb_checklists=Test_check kb_reference=Test_ref atc_id=G-AEXT atc_id_color=0x00000000 ui_manufacturer=Dart ui_type=Kitten II ui_variation=G-AEXT description=DART KITTEN II - G-AEXT (1937) The Kitten was built by glider builders Alfred R.Weyl and Erich P.Zander under the name of Dart Aircraft Ltd at their premises in Dunstable, flying for the first time in April 1937. This aircraft is a single-seat, low-wing ultra-light monoplane, one of only 3 factory built examples (designated I, II and III respectively) and the only known survivor. Dart Kitten II had a more powerful motor (36 h.p. Aeronca-J.A.P. J-99 ) than its older sibling, along with minor revisions to the airframe and undercarriage. After the war Weyl and Zander continued to build gliders as the Hawkridge Aircraft Company until the business was dissolved in 1952. visual_damage=0 atc_heavy=0 atc_id_font=Verdana,100,1,600,0 [fltsim.1] title=Dart Kitten II Race G-AMJP sim=DartKitten model= panel= sound= texture=mjp checklists= kb_checklists=Test_check kb_reference=Test_ref atc_id=G-AMJP atc_id_color=0x00000000 ui_manufacturer=Dart ui_type=Kitten II ui_variation=G-AMJP description=DART KITTEN II - G-AEXT (1937) The Kitten was built by glider builders Alfred R.Weyl and Erich P.Zander under the name of Dart Aircraft Ltd at their premises in Dunstable, flying for the first time in April 1937. This aircraft is a single-seat, low-wing ultra-light monoplane, one of only 3 factory built examples (designated I, II and III respectively) and the only known survivor. Dart Kitten II had a more powerful motor (36 h.p. Aeronca-J.A.P. J-99 ) than its older sibling, along with minor revisions to the airframe and undercarriage. After the war Weyl and Zander continued to build gliders as the Hawkridge Aircraft Company until the business was dissolved in 1952. visual_damage=0 atc_heavy=0 atc_id_font=Verdana,100,1,600,0 [General] atc_type=Dart atc_model=Dart editable=1 performance=General characteristics\n \nCrew: 1 \nCapacity: 1 \nLength: 21 ft 4 in ( m) \nWingspan: 31 ft 9 in ( m) \nHeight: 7 ft 11 in ( m) \nEmpty weight: 582 lb ( kg) \nGross weight: 860 lb ( kg) \nPowerplant: 1 × Aeronca-J.A.P. J-99 two-cylinder aircooled, 40 hp ( kW)\n \nPerformance\n \nMaximum speed: 95 mph ( km/h) \nCruise speed: 83 mph ( km/h) \nRange: 340 miles ( km) \nService ceiling: 19,700 ft ( m) category=airplane [weight_and_balance] // ACM V2.5 max_gross_weight =1220.0 empty_weight =680.00000 reference_datum_position = 0.700, 0.000, 0.000 empty_weight_CG_position = 0.000, 0.000, 0.000 empty_weight_pitch_MOI =376.00000 empty_weight_roll_MOI =370.00000 empty_weight_yaw_MOI =622.00000 empty_weight_coupled_MOI =0.00000 max_number_of_stations =0 [lights] //Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing //light.0 =4, -1.100000, 0.000000, 1.500000, fx_vclightwhi [GeneralEngineData] //0=Piston, 1=Jet, 2=None, 3=Helo-Turbine, 4=Rocket, 5=Turboprop engine_type =0 fuel_flow_scalar =1.00000 min_throttle_limit =0.00000 engine.0 =3.200, 0.000, 0.500 [effects] wake = fx_wake water = fx_spray dirt = fx_tchdrt concrete = fx_sparks touchdown = fx_tchdwn_s, 1 startup = fx_engstrt_cub windshield_rain_effect_available = 1 [fuel] //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons) fuel_type =1 number_of_tank_selectors =1 electric_pump =0 Center1 = 1.000, 0.000, 0.000, 12.000, 0.000 fuel_dump_rate=0.02000 anemometer_pump=0 manual_pump=0 engine_driven_pump=0 [contact_points] static_pitch = 13.160 static_cg_height = 4.620 tailwheel_lock =0 gear_system_type =0 max_number_of_points =3 point.0= 1, -14.640, 0.000, -1.536, 1600, 0, 0.238, 60.000, 0.200, 2.500, 0.800, 0.000, 0.000, 0 point.1= 1, 1.130, -3.100, -5.000, 1600, 1, 0.790, 0.000, 0.200, 2.500, 0.800, 0.000, 0.000, 2 point.2= 1, 1.130, 3.100, -5.000, 1600, 2, 0.790, 0.000, 0.200, 2.500, 0.800, 0.000, 0.000, 3 [keyboard_response] elevator = 200, 1000 aileron = 200, 1000 rudder = 200, 1000 //Delta on the amount of brake when the rudder pedals deflected [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 =500 gear_bump_right_duration =250000 ground_bumps_magnitude1 =3250 ground_bumps_angle1 =8900 ground_bumps_intercept1 =5 ground_bumps_slope1 =0.48 ground_bumps_magnitude2 =750 ground_bumps_angle2 =9100 ground_bumps_intercept2 =0.075 ground_bumps_slope2 =1 crash_magnitude1 =10000 crash_direction1 =1000 crash_magnitude2 =10000 crash_direction2 =9000 crash_period2 =75000 crash_duration2 =2500000 stick_shaker_magnitude =5000 stick_shaker_direction =0 stick_shaker_period =111111 [airplane_geometry] //ACM_AREAW1// 0,0,0,1.6002,0.5960,0.5960,0,1.5197,1.1921,1.1921 //ACM_AREAW2// 0,1.4400,1.7881,1.7881,0,1.3601,2.3842,2.3842,0,1.2798 //ACM_AREAW3// 2.9802,2.9802,0,1.2000,3.5762,3.5762,0,1.1201,4.1722,4.1722 //ACM_AREAW4// 0,1.0398,4.7684,4.7684,0,0.9599,5.3642,5.3642,0,0.8801 //ACM_AREAH1// 0,0,0,0.9753,0.1624,0.1624,0.0938,1.0204,0.3251,0.3251 //ACM_AREAH2// 0.1877,1.0655,0.4875,0.4875,0.2815,1.1102,0.6502,0.6502,0.3754,1.1555 //ACM_AREAH3// 0.8126,0.8126,0.4690,1.2007,0.9753,0.9753,0.5630,1.2458,1.1375,1.1375 //ACM_AREAH4// 0.6567,1.2905,1.3004,1.3004,0.7508,1.3358,1.4630,1.4630,0.8446,1.3811 //ACM_AREAV1// 0,0,0,1.3530,0.1500,0.1500,0.1172,1.3624,0.3007,0.3007 //ACM_AREAV2// 0.2345,1.3717,0.4510,0.4510,0.3524,1.3809,0.6014,0.6014,0.4699,1.3901 //ACM_AREAV3// 0.7518,0.7518,0.5874,1.3990,0.9021,0.9021,0.7048,1.4084,1.0525,1.0525 //ACM_AREAV4// 0.8223,1.4177,1.2029,1.2029,0.9398,1.4270,1.3530,1.3530,1.0571,1.4362 //ACM_CAREAW1// 2.6821,2.6821,0.8001,1.1201,2.9802,2.9802,0.8001,1.1038,3.2781,3.2781 //ACM_CAREAW2// 0.8001,1.0880,3.5762,3.5762,0.8001,1.0721,3.8743,3.8743,0.8001,1.0561 //ACM_CAREAW3// 4.1722,4.1722,0.8001,1.0398,4.4703,4.4703,0.8001,1.0240,4.7684,4.7684 //ACM_CAREAW4// 0.8001,1.0081,5.0664,5.0664,0.8001,0.9921,5.3642,5.3642,0.8001,0.9761 //ACM_CAREAH1// 0,0,0.4875,0.9753,0.1624,0.1624,0.5813,1.0448,0.3251,0.3251 //ACM_CAREAH2// 0.6753,1.1143,0.4875,0.4875,0.7692,1.1835,0.6502,0.6502,0.8629,1.2532 //ACM_CAREAH3// 0.8126,0.8126,0.9569,1.3227,0.9753,0.9753,1.0506,1.3918,1.1375,1.1375 //ACM_CAREAH4// 1.1446,1.4615,1.3004,1.3004,1.2381,1.5311,1.4630,1.4630,1.3322,1.6002 //ACM_CAREAV1// 0,0,0.3382,1.0147,0.1500,0.1500,0.4557,1.0779,0.3007,0.3007 //ACM_CAREAV2// 0.5730,1.1416,0.4510,0.4510,0.6905,1.2050,0.6014,0.6014,0.8082,1.2683 //ACM_CAREAV3// 0.7518,0.7518,0.9257,1.3315,0.9021,0.9021,1.0432,1.3947,1.0525,1.0525 //ACM_CAREAV4// 1.1605,1.4584,1.2029,1.2029,1.2781,1.5217,1.3530,1.3530,1.3954,1.5851 wing_area =178.50000 wing_span =35.20000 wing_root_chord =5.25000 wing_dihedral =1.10000 wing_incidence =0.00000 wing_twist =0.00000 oswald_efficiency_factor =0.60000 wing_winglets_flag =0 wing_sweep =0.00000 wing_pos_apex_lon =1.30988 wing_pos_apex_vert =2.10000 htail_area =18.20000 htail_span =9.60000 htail_pos_lon =-13.40000 htail_pos_vert =1.30000 htail_incidence =0.00000 htail_sweep =30.00000 vtail_area =13.00000 vtail_span =4.44000 vtail_sweep =38.00000 vtail_pos_lon =-13.50000 vtail_pos_vert =1.60000 elevator_area =10.64000 aileron_area =9.60000 rudder_area =6.55000 elevator_up_limit =30.00000 elevator_down_limit =20.00000 aileron_up_limit =20.00000 aileron_down_limit =20.00000 rudder_limit =28.00000 elevator_trim_limit =10.00000 spoiler_limit =0.00000 aileron_to_spoileron_gain =0.00000 spoiler_handle_available =0 min_ailerons_for_spoilerons =0.00000 min_flaps_for_spoilerons =0.00000 spoilerons_available =0 spoiler_extension_time=0.00000 auto_spoiler_available=0 positive_g_limit_flaps_up=3.70000 negative_g_limit_flaps_up=-2.96000 positive_g_limit_flaps_down=2.59000 negative_g_limit_flaps_down=-2.22000 load_safety_factor=1.00000 [electrical] max_battery_voltage = 0 generator_alternator_voltage = 0 max_generator_alternator_amps = 60 engine_generator_map = 1 electric_always_available = 0 [flight_tuning] cruise_lift_scalar=1.00000 parasite_drag_scalar=1.00000 induced_drag_scalar=1.00000 elevator_effectiveness=1.00000 aileron_effectiveness=1.00000 rudder_effectiveness=1.00000 pitch_stability=1.00000 roll_stability=1.00000 yaw_stability=1.00000 elevator_trim_effectiveness=1.00000 aileron_trim_effectiveness=1.00000 rudder_trim_effectiveness=1.00000 p_factor_on_yaw =0.30000 torque_on_roll =0.30000 gyro_precession_on_yaw =0.30000 gyro_precession_on_pitch = 0.3 hi_alpha_on_roll=1.00000 hi_alpha_on_yaw=1.00000 gyro_precession_on_roll=1.00000 [piston_engine] power_scalar=1.00000 cylinder_displacement=42.75000 compression_ratio=7.50000 number_of_cylinders=4 max_rated_rpm=2300.00000 max_rated_hp=65.00000 fuel_metering_type=1 cooling_type=0 normalized_starter_torque=0.33575 turbocharged=0 max_design_mp=29.92000 min_design_mp=2.99200 critical_altitude=0.00000 emergency_boost_type=0 emergency_boost_mp_offset=0.00000 emergency_boost_gain_offset=0.00000 fuel_air_auto_mixture=0 auto_ignition=0 max_rpm_mechanical_efficiency_scalar=1.00000 idle_rpm_mechanical_efficiency_scalar=1.00000 max_rpm_friction_scalar=1.00000 idle_rpm_friction_scalar=1.00000 emergency_boost_duration=0.00000 BestPowerSpecificFuelConsumption=0.50000 detonation_onset=32.91000 [propeller] thrust_scalar=1.00000 propeller_type=1 propeller_diameter=6.00000 propeller_blades=2 propeller_moi=3.86478 beta_max=14.75000 beta_min=12.75000 min_gov_rpm=0.00000 prop_tc=0.10000 gear_reduction_ratio=1.00000 fixed_pitch_beta=13.75000 low_speed_theory_limit=80.00000 prop_sync_available=0 prop_deice_available=0 prop_feathering_available=0 prop_auto_feathering_available=0 min_rpm_for_feather=0.00000 beta_feather=0.00000 power_absorbed_cf=0.00000 defeathering_accumulators_available=0 prop_reverse_available=0 minimum_on_ground_beta=0.00000 minimum_reverse_beta=0.00000 [brakes] parking_brake =1 toe_brakes_scale =0.50000 differential_braking_scale =1.00000 auto_brakes=0 hydraulic_system_scalar=0.00000 [hydraulic_system] normal_pressure =0.00000 engine_map=1,0,0,0 [Views] eyepoint=-1.800, 0.000, 0.800 [Radios] // Radio Type = availiable, standby frequency, has glide slope Audio.1=0 Com.1=1, 0 Nav.1=0, 0, 0 Adf.1=0 Transponder.1=0 Marker.1=0 [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=0,0 [attitude_indicators] //Type: 0=None, 1=Vacuum Gyro, 2=Electric Gyro attitude_indicator.0 = 0 [turn_indicators] //Type: 0=None, 1=Electric Gyro, 2= Vacuum Gyro turn_indicator.0=0,0 [Reference Speeds] flaps_up_stall_speed=33.0 //Knots True (KTAS) full_flaps_stall_speed=33.0 //Knots True (KTAS) cruise_speed=54.74552 max_indicated_speed =129.99890 max_mach=0.13800 [autopilot] autopilot_available=0 flight_director_available=0 yaw_damper_gain=0 default_vertical_speed=1000 default_pitch_mode=0 default_bank_mode=0 autothrottle_available=0 autothrottle_arming_required=0 autothrottle_takeoff_ga=1 autothrottle_max_rpm=90 max_throttle_rate=0.1 pitch_takeoff_ga=8 max_pitch=10 max_pitch_acceleration=1 max_pitch_velocity_lo_alt=2 max_pitch_velocity_hi_alt=1.5 max_pitch_velocity_lo_alt_breakpoint=20000 max_pitch_velocity_hi_alt_breakpoint=28000 max_bank=25 max_bank_acceleration=1.8 max_bank_velocity=3 nav_proportional_control=9 nav_integrator_control=0.25 nav_derivative_control=0 nav_integrator_boundary=2.5 nav_derivative_boundary=0 gs_proportional_control=9.52 gs_integrator_control=0.26 gs_derivative_control=0 gs_integrator_boundary=0.7 gs_derivative_boundary=0 use_no_default_bank=1 use_no_default_pitch=1 [stall_warning] type=0 //0=Fuel Injected, 1=Gravity Carburetor, 2=Aerobatic Carburetor stick_shaker=1 [GPWS] max_warning_height=0 sink_rate_fpm=-1500 excessive_sink_rate_fpm=-2000 climbout_sink_rate_fpm=-100 flap_and_gear_sink_rate_fpm=-100 [pneumatic_system] max_pressure=18 bleed_air_scalar=0.15 [deice_system] structural_deice_type=0 [vacuum_system] max_pressure=5.15 vacuum_type=0 electric_backup_pressure=0 engine_map=1, 0, 0, 0 [gear_warning_system] gear_warning_available=0 pct_throttle_limit=0.00000 flap_limit_idle=0.00000 flap_limit_power=0.00000 [AirWrench] Aircraft_Length=28.16000 Vmax_sl=82.20000 Vmax_ca=82.20000 V_si=29.50000 V_so=29.50000 V_rc=31.20000 Climb_Rate=948.60000 Climb_Weight=752.00000 Max_gforce=3.70000 Emergency_hp=65.00000 VSI_Weight=680.00000 static_margin=0.11000 nose_position_lon=8.31000 ActualIncidence=2.50000 ActualTwist=-1.00000 ActualTailIncidence=-0.80000 Aircraft_Type=2 ReheatCutoff=1.20000 OptimumMach=0.90000 Power_Calibration=1.00000 IdleRPM=575.00000 piston_research=0.00000 Max_Prop_Eff=0.85000 JetAltitude=0.00000 turboprop_critical_altitude=0.00000 target_roll_Vopt=523.20000 target_roll_rate=129.00000 zero_roll_mph=750.00000 pitch_damping=1.00000 yaw_damping=0.00000 roll_damping=1.00000 weathervane=1.00000 elevator_scalar=1.00000 aileron_scalar=1.00000 rudder_scalar=1.00000 dihedral_scalar=1.00000 sideslip_scalar=1.00000 prop_yaw_damping_scalar=1.00000 Elevator_FF=130.00000 Aileron_FF=-150.00000 Roll_Response=30.00000 Adverse_Yaw=100.00000 Control_Response=100.00000 V_Max_Control=121.98257 V_Zero_Control=243.96515 V_Max_RdrControl=122.00000 V_Zero_RdrControl=244.00000 Spin_Stability=100.00000 Roll_Off=0.00000 glide_ratio=6.47067 vn_gmax=3.65625 vn_vmo=121.98257 expert_mode=0 CritAoA=16.00000 ClAoA_k0=1.00000 ClAoA_k1=1.00000 ClAoA_k2=0.85000 ClAoA_k3=0.80000 cruise_attitude=0.00000 Elevator_Propwash=1.00000 Rudder_Propwash=1.00000 afterburner_thrust=0.00000 prop_design_altitude=5000.00000 prop_material_type=1 protect_airfile=0 spoiler_type=0 spoiler_cd=0.00000 spoiler_cl=0.00000 spoiler_cm=0.00000 auto_flaps_enabled=0 flaps_type=0 flaps_cd_scalar=0.00000 flaps_cm_scalar=-0.00000 vfe_enabled=0 gear_cd_scalar=0.00000 gear_cm_scalar=-0.00000 critical_mach_number=0.80000 max_mach_cd0=60 cylinder_head_temperature=501.00000 exhaust_gas_temperature=1201.00000 fuel_pressure=16.50000 oil_pressure=60.00000 oil_temperature=241.00000 radiator_temperature=211.00000 lo_rpm_friction=1.00000 hi_rpm_friction=1.00000 exhaust_pressure_ratio=0.00000 interstage_turbine_temperature=-459.00000 RAM_Jet_Effect=1.00000 Emulate_Turbojet=0 N2_idle=66.00000 jet_idle_scalar=1.00000 input_units=0 fs_version=5 AI_flag=0 edit_tp_torque=0 keep_jet_air_defs=0 direct_edit_mach=0 direct_edit_2dtab=0 fixed_wing_pos=0 range_est_alt=0.00000 range_est_rpm=2300.00000 range_est_mp=29.92000 range_est_fuel=12.00000 contact_light_flags=0 AirWrenchVersion=1.01.83 [pitot_static] pitot_heat=1.000000 [Flaps.0] type=0 span-outboard=0.500000 extending-time=0.000000 system_type=0
