[fltsim.0] title=Gladiator MkII (RNLAF) sim=Gloster Gladiator Mk2 model= panel= sound= texture=RNLAF kb_checklists= ui_manufacturer=Gloster ui_type=Gladiator MkII ui_variation=RNLAF description=The Gloster GladiatorMk 2 was the last British biplane fighter, a development of the Gauntlet with an enclosed single seat cockpit, cantilever landing gear and with increased armament, and a 3 blade fixed pitch propeller. First flown in 1935, the Gladiator went into service with the RAF in 1936. The Mark II a 830 hp Bristol Mercury VIIIA engine. atc_id_color=0000000000 visual_damage=0 [weight_and_balance] // ACM V2.3 max_gross_weight = 4882.9 empty_weight = 3645 reference_datum_position = 0, 0, 0 empty_weight_CG_position = 0.3, 0, 0 empty_weight_pitch_MOI = 2295 empty_weight_roll_MOI = 1660 empty_weight_yaw_MOI = 3621 empty_weight_coupled_MOI = 0 max_number_of_stations = 1 station_load.0 = 200, -5.210, 0.000, 0.000 [lights] //Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing light.0 = 3, 1.90, -13.50, 4.07, fx_navredsml light.1 = 3, -21.51, -0.06, 0.74, fx_navwhisml light.2 = 3, 1.96, 13.43, 4.13, fx_navgresml [GeneralEngineData] //0=Piston, 1=Jet, 2=None, 3=Helo-Turbine, 4=Rocket, 5=Turboprop engine_type = 0 fuel_flow_scalar = 1.00000 engine.0 = 5.000, 0.000, 0.000 min_throttle_limit=0.000000 [fuel] //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons) fuel_type = 1 number_of_tank_selectors = 1 Center1 = 0, 0, 0.1, 99, 0 electric_pump=1 [contact_points] static_pitch = 13.3 static_cg_height = 6.438 tailwheel_lock = 0 max_number_of_points = 7 point.0 = 1, -16.300, 0.000, -3.200, 3200, 0, 0.300, 0.000, 0.400, 2.500, 0.500, 0.000, 0.000, 0 point.1 = 1, 2.4566, -2.96, -7.1, 2200, 1, 1.05, 0, 0.5, 2.5, 0.83, 0, 0, 2, 0, 0 point.2 = 1, 2.41, 2.96, -7.1, 2200, 2, 1.05, 0, 0.5, 2.5, 0.83, 0, 0, 3, 0, 0 point.3 = 2, 0.000, -17.080, -2.500, 1200, 0, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 5 point.4 = 2, 0.000, 17.080, -2.500, 1200, 0, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 6 point.5 = 2, -16.660, 0.000, -1.660, 2400, 0, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 9 point.6 = 2, 7.910, 0.000, -2.000, 1200, 0, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 4 [keyboard_response] elevator = 350.000000, 500.000000 aileron = 450.000000, 1000.000000 rudder = 200.000000, 1000.000000 [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 = 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// 0,0,0,1.5240,0.5460,0.5460,0,1.4478,1.0921,1.0921 //ACM_AREAW2// 0,1.3716,1.6382,1.6382,0,1.2954,2.1843,2.1843,0,1.2192 //ACM_AREAW3// 2.7304,2.7304,0,1.1430,3.2765,3.2765,0,1.0667,3.8226,3.8226 //ACM_AREAW4// 0,0.9906,4.3687,4.3687,0,0.9144,4.9148,4.9148,0,0.8382 //ACM_AREAH1// 0,0,0,1.2530,0.2088,0.2088,0,1.1904,0.4176,0.4176 //ACM_AREAH2// 0,1.1277,0.6265,0.6265,0,1.0651,0.8353,0.8353,0,1.0024 //ACM_AREAH3// 1.0442,1.0442,0,0.9397,1.2530,1.2530,0,0.8771,1.4619,1.4619 //ACM_AREAH4// 0,0.8144,1.6707,1.6707,0,0.7518,1.8795,1.8795,0,0.6891 //ACM_AREAV1// 0,0,0,1.7272,0.1919,0.1919,0,1.5890,0.3838,0.3838 //ACM_AREAV2// 0,1.4508,0.5757,0.5757,0,1.3126,0.7676,0.7676,0,1.1744 //ACM_AREAV3// 0.9595,0.9595,0,1.0363,1.1514,1.1514,0,0.8981,1.3433,1.3433 //ACM_AREAV4// 0,0.7599,1.5352,1.5352,0,0.6217,1.7272,1.7272,0,0.4836 //ACM_CAREAW1// 2.4574,2.4574,0.7620,1.0667,2.7304,2.7304,0.7620,1.0515,3.0035,3.0035 //ACM_CAREAW2// 0.7620,1.0363,3.2765,3.2765,0.7620,1.0210,3.5496,3.5496,0.7620,1.0058 //ACM_CAREAW3// 3.8226,3.8226,0.7620,0.9906,4.0957,4.0957,0.7620,0.9753,4.3687,4.3687 //ACM_CAREAW4// 0.7620,0.9601,4.6418,4.6418,0.7620,0.9448,4.9148,4.9148,0.7620,0.9296 //ACM_CAREAH1// 0,0,0.6265,1.2530,0.2088,0.2088,0.6265,1.2217,0.4176,0.4176 //ACM_CAREAH2// 0.6265,1.1904,0.6265,0.6265,0.6265,1.1590,0.8353,0.8353,0.6265,1.1277 //ACM_CAREAH3// 1.0442,1.0442,0.6265,1.0964,1.2530,1.2530,0.6265,1.0651,1.4619,1.4619 //ACM_CAREAH4// 0.6265,1.0337,1.6707,1.6707,0.6265,1.0024,1.8795,1.8795,0.6265,0.9711 //ACM_CAREAV1// 0,0,0.4318,1.2954,0.1919,0.1919,0.4318,1.2263,0.3838,0.3838 //ACM_CAREAV2// 0.4318,1.1572,0.5757,0.5757,0.4318,1.0881,0.7676,0.7676,0.4318,1.0190 //ACM_CAREAV3// 0.9595,0.9595,0.4318,0.9499,1.1514,1.1514,0.4318,0.8808,1.3433,1.3433 //ACM_CAREAV4// 0.4318,0.8117,1.5352,1.5352,0.4318,0.7426,1.7272,1.7272,0.4318,0.6736 wing_area = 323.00000 wing_span = 32.25000 wing_root_chord = 5.00000 wing_dihedral = 3.00000 wing_incidence = 0.00000 wing_twist = 0.00000 oswald_efficiency_factor = 0.88000 wing_winglets_flag = 0 wing_sweep = 0.00000 wing_pos_apex_lon = 2.50388 wing_pos_apex_vert = 0.00000 htail_area = 40.00000 htail_span = 12.33333 htail_pos_lon = -16.41667 htail_pos_vert = 0.00000 htail_incidence = 0.00000 htail_sweep = 0.00000 vtail_area = 24.00000 vtail_span = 5.66667 vtail_sweep = 0.00000 vtail_pos_lon = -16.66667 vtail_pos_vert = 0.00000 elevator_area = 22.30000 aileron_area = 23.30000 rudder_area = 15.20000 elevator_up_limit = 20.00000 elevator_down_limit = 20.00000 aileron_up_limit = 15.00000 aileron_down_limit = 15.00000 rudder_limit = 25.00000 elevator_trim_limit = 18.00000 spoiler_limit = 0.00000 aileron_to_spoileron_gain = 0.00000 min_ailerons_for_spoilerons = 0.00000 min_flaps_for_spoilerons = 0.00000 spoilerons_available = 0 [electrical] max_battery_voltage = 24 generator_alternator_voltage = 28 max_generator_alternator_amps = 160 electric_always_available = 1 flap_motor = 0, 5, 17 gear_motor = 0, 5, 17 autopilot = 0, 5, 17 avionics_bus = 0, 10, 17 avionics = 1, 5, 17 pitot_heat = 0, 2, 17 additional_system = 0, 20, 17 marker_beacon = 1, 2, 17 gear_warning = 0, 2, 17 fuel_pump = 0, 5, 17 starter1 = 0, 20, 17 starter2 = 0, 20, 17 starter3 = 0, 20, 17 starter4 = 0, 20, 17 light_nav = 0, 5, 17 light_beacon = 0, 5, 17 light_landing = 0, 5, 17 light_taxi = 0, 5, 17 light_strobe = 0, 5, 17 light_panel = 0, 5, 17 prop_sync = 0, 15, 17 auto_feather = 0, 15, 17 auto_brakes = 0, 15, 17 standby_vacuum = 0, 15, 17 hydraulic_pump = 0, 2, 17 fuel_transfer_pump = 0, 5, 17 propeller_deice = 0, 5, 17 light_recognition = 0, 5, 17 light_wing = 0, 5, 17 light_logo = 0, 5, 17 [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 hi_alpha_on_roll =1.00000 hi_alpha_on_yaw =1.00000 p_factor_on_yaw =1.00000 torque_on_roll =1.00000 gyro_precession_on_roll =1.00000 gyro_precession_on_yaw =1.00000 [piston_engine] power_scalar=1.00000 cylinder_displacement=168.88889 compression_ratio=7.00000 number_of_cylinders=9 max_rated_rpm=2750.00000 max_rated_hp=830.00000 fuel_metering_type=2 cooling_type=0 normalized_starter_torque=0.03498 turbocharged=1 max_design_mp=50.00000 min_design_mp=9.00000 critical_altitude=14500.00000 emergency_boost_type=0 emergency_boost_mp_offset=0.00000 emergency_boost_gain_offset=0.00000 fuel_air_auto_mixture=0 auto_ignition=0 emergency_boost_duration=300.00000 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 [propeller] thrust_scalar=1.00000 propeller_type=1 propeller_diameter=10.5 propeller_blades=3 propeller_moi=36.10000 beta_max=31.00000 beta_min=29.00000 min_gov_rpm=360.00000 prop_tc=0.01000 gear_reduction_ratio=2.07000 fixed_pitch_beta=30.00000 low_speed_theory_limit=80.00000 prop_sync_available=0 prop_deice_available=1 prop_feathering_available=0 prop_auto_feathering_available=0 min_rpm_for_feather=700.00000 beta_feather=88.50000 power_absorbed_cf=0.90000 defeathering_accumulators_available=0 prop_reverse_available=0 minimum_on_ground_beta=1.00000 minimum_reverse_beta=-14.00000 rotation = -1 [folding_wings] wing_fold_system_type = 4 fold_rates = 0.12, 0.11 [TailHook] tailhook_length = 4 tailhook_position = -15, 0, -1 cable_force_adjust = 1 [Views] eyepoint=-5.252313, 0, 2.934814 [flaps.0] //Trailing Edge Flaps type = 1 span-outboard = 0.5 extending-time = 5 flaps-position.0 = 0 flaps-position.1 = 11, 139 flaps-position.2 = 22, 133 flaps-position.3 = 33, 127 flaps-position.4 = 45, 121 damaging-speed = 139 blowout-speed = 151 [LSO] LSOAdjustSpeed = 1.2 [exits] number_of_exits = 1 exit_rate.0 = 0.4 [General] performance=+ Weight: 3845 lbs Max 4864 lbs + Power: 830 hp MIL 830 hp WEP + 6.0g Corner speed: 140 mph + Max speed @ SL: 242 mph + Max speed: 257 mph @ 14500 ft + Climb rate: 1475 ft/min @ 92 mph Flight Dynamics By: C Bielat thicko FD Build 5 - 7/6/06 06:59 PM Flight Dynamics Workbook V2.84.50 editable=1 [brakes] toe_brakes_scale=0.64089 [gear_warning_system] gear_warning_available=0 pct_throttle_limit=0.00000 flap_limit_idle=33.75000 flap_limit_power=16.87500 [Reference Speeds] flaps_up_stall_speed=53.00755 full_flaps_stall_speed=53.00755 cruise_speed=168.75518 max_indicated_speed=304.00000 max_mach=0.34700 [autopilot] autopilot_available=1 flight_director_available=0 autothrottle_available=0 autothrottle_arming_required=0 default_pitch_mode=0 default_bank_mode=0 use_no_default_bank=1 use_no_default_pitch=1 default_vertical_speed=1000.00000 autothrottle_takeoff_ga=1.00000 autothrottle_max_rpm=90.00000 pitch_takeoff_ga=8.00000 max_pitch=10.00000 max_pitch_acceleration=1.00000 max_pitch_velocity_lo_alt=2.00000 max_pitch_velocity_hi_alt=1.50000 max_pitch_velocity_lo_alt_breakpoint=20000.00000 max_pitch_velocity_hi_alt_breakpoint=28000.00000 max_bank=25.00000 max_bank_acceleration=1.80000 max_bank_velocity=3.00000 max_throttle_rate=0.10000 nav_proportional_control=9.00000 nav_integrator_control=0.25000 nav_derivative_control=0.00000 nav_integrator_boundary=2.50000 nav_derivative_boundary=0.00000 gs_proportional_control=9.52000 gs_integrator_control=0.26000 gs_derivative_control=0.00000 gs_integrator_boundary=0.70000 gs_derivative_boundary=0.00000 yaw_damper_gain=0.00000 [hydraulic_system] normal_pressure=998.00000 engine_map=1,0,0,0 [AirWrench] Aircraft_Length=27.41250 Vmax_sl=242.80000 Vmax_ca=263.90000 V_rc=85.10000 Climb_Rate=1376.80000 Climb_Weight=4439.00000 Max_gforce=6.00000 Emergency_hp=830.00000 nose_position_lon=9.59437 ActualIncidence=0.00000 ActualTwist=0.00000 ActualTailIncidence=0.00000 Aircraft_Type=2 FlowCorrection=1.00000 Power_Correction=1.00000 JetAltitude=0.00000 turboprop_critical_altitude=0.00000 target_roll_Vopt=148.30000 target_roll_rate=83.60000 pitch_damping=1.00000 yaw_damping=1.00000 elevator_scalar=1.00000 rudder_scalar=1.00000 dihedral_scalar=1.00000 Elevator_FF=50.00000 Aileron_FF=-50.00000 Roll_Response=30.00000 Adverse_Yaw=100.00000 Control_Response=100.00000 V_Max_Control=349.83682 V_Zero_Control=699.67363 Spin_Stability=100.00000 Stall_Stability=100.00000 Elevator_Propwash=1.00000 Rudder_Propwash=1.00000 spoiler_time=1.00000 afterburner_thrust=0.00000 mach_scale=1.00000 spoiler_type=1 spoiler_cd=0.00000 spoiler_cl=0.00000 spoiler_cm=0.00000 flaps_type=1 flaps_cd_scalar=0.93200 flaps_cm_scalar=0.39300 vfe_enabled=0 gear_cd_scalar=0.00000 gear_cm_scalar=0.00000 cylinder_head_temperature=501.00000 exhaust_gas_temperature=1201.00000 fuel_pressure=20.00000 oil_pressure=60.00000 oil_temperature=241.00000 radiator_temperature=211.00000 exhaust_pressure_ratio=0.00000 interstage_turbine_temperature=-459.00000 knots_flag=0 cfs1_flag=0 laminar_flow=0 fixed_wing_pos=0 AirWrenchVersion=1.01.31 [stall_warning] type=1 [attitude_indicators] attitude_indicator.0=1 [turn_indicators] turn_indicator.0=1,0 [direction_indicators] direction_indicator.0=1,0 [SMOKESYSTEM] smoke.0=0.00, 12.5, 0.0, Maraud_1.fx // gunner sound smoke.1=0.00, 11.1,-5.60, Maraud_2.fx //Fronside l dn smoke.2=0.00, 11.1, 5.60, Maraud_2.fx //Fronside r dn moke.1=0.00, 9.0,-0.0, Maraud_4.fx //Bowgunner smoke.3=0.0,4750.00,0.00, fx_ShellHit
