[fltsim.0] title=VP-1 green sim=VP-1 model = panel = sound = texture = panel_alias = sound_alias = kb_checklists = kb_reference = atc_id =N402PB atc_id_color = atc_parking_types = atc_parking_code = ui_manufacturer = Evans (Homebuilt) ui_type = VP-1 ui_variation = US Civil Register Green/Grey description = Homebuilt Light Sporting Aircraft [fltsim.1] title=VP-1 yellow sim=VP-1 model = panel = sound = texture =yellow panel_alias = sound_alias = kb_checklists = kb_reference = atc_id =N279TC atc_id_color = atc_parking_types = atc_parking_code = ui_manufacturer = Evans (Homebuilt) ui_type = VP-1 ui_variation = US Civil Register Green/Yellow description = Homebuilt Light Sporting Aircraft [General] atc_type = atc_model = EVANS editable = 1 visual_damage=1 performance = + Empty Weight: 640 lbs + Max Power: 60 Hp + Maneuver speed: 81 mph @ 4.0 g + Max speed: 115 mph @ 5000 ft + Max speed at sea-level: 114 mph + Climb rate: 1000 ft/min @ 56 mph Flight Dynamics By: Tim Piglet Conrad Piglet's Peculiar Planes FD Build 4 - 7/21/04 05:22 AM Flight Dynamics Workbook V2.84.65 [pitot_static] vertical_speed_time_constant = 2 [WEIGHT_AND_BALANCE] max_gross_weight = 750 empty_weight = 440 reference_datum_position = 0, 0, 0 empty_weight_CG_position = -0.01, 0, 0 CG_forward_limit = 0 CG_aft_limit = 1 max_number_of_stations = 13 station_load.0 = 200, -0.6, 0, 0, Pilot empty_weight_pitch_MOI = 185 empty_weight_roll_MOI = 96 empty_weight_yaw_MOI = 263 empty_weight_coupled_MOI = 0 [flight_tuning] cruise_lift_scalar = 1 parasite_drag_scalar = 1 induced_drag_scalar = 1 elevator_effectiveness = 1 aileron_effectiveness = 1 rudder_effectiveness = 1 pitch_stability = 1 roll_stability = 1 yaw_stability = 1 elevator_trim_effectiveness = 1 aileron_trim_effectiveness = 1 rudder_trim_effectiveness = 1 hi_alpha_on_roll = 1 hi_alpha_on_yaw = 1 p_factor_on_yaw = 1 torque_on_roll = 1 gyro_precession_on_roll = 1 gyro_precession_on_yaw = 1 [GeneralEngineData] engine_type = 0 Engine.0 = 4.37, 0, 0 fuel_flow_scalar = 1 min_throttle_limit = 0 [piston_engine] power_scalar = 1 cylinder_displacement = 24.408 compression_ratio = 8 number_of_cylinders = 4 max_rated_rpm = 3600 max_rated_hp = 60 fuel_metering_type = 1 cooling_type = 0 normalized_starter_torque = 0.342 turbocharged = 0 max_design_mp = 29.9 min_design_mp = 9 critical_altitude = 5000 emergency_boost_type = 0 emergency_boost_mp_offset = 0 emergency_boost_gain_offset = 0 fuel_air_auto_mixture = 0 auto_ignition = 0 emergency_boost_duration = 0 max_rpm_mechanical_efficiency_scalar = 1 idle_rpm_mechanical_efficiency_scalar = 1 max_rpm_friction_scalar = 1 idle_rpm_friction_scalar = 1 [propeller] thrust_scalar = 1 propeller_type = 1 propeller_diameter = 4.5 propeller_blades = 2 propeller_moi = 1.8 beta_max = 35 beta_min = 15 min_gov_rpm = 540 prop_tc = 0.01 gear_reduction_ratio = 1 fixed_pitch_beta = 25 low_speed_theory_limit = 59.5188260334892 prop_sync_available = 0 prop_deice_available = 1 prop_feathering_available = 0 prop_auto_feathering_available = 0 min_rpm_for_feather = 700 beta_feather = 88.5 power_absorbed_cf = 0.9 defeathering_accumulators_available = 0 prop_reverse_available = 0 minimum_on_ground_beta = 1 minimum_reverse_beta = -14 rotation = -1 [contact_points] max_number_of_points = 7 point.0 = 1, -12.606, 0, -1.35, 2200, 0, 0.33, 30, 0.2, 2.0, 0.95, 0, 0, 0, 0, 0 point.1 = 1, 1, -2.407, -3.38, 2200, 1, 0.8, 0, 0.3, 2.5, 0.501, 0, 0, 2, 0, 0 point.2 = 1, 1, 2.407, -3.38, 2200, 2, 0.8, 0, 0.3, 2.5, 0.501, 0, 0, 3, 0, 0 point.3 = 2, 3.586, 0, -0.968, 1200, 0, 0, 0, 0, 0, 0, 0, 0, 4 point.4 = 2, -11.845, 0, -0.426, 1200, 0, 0, 0, 0, 0, 0, 0, 0, 9 point.5 = 2, 0, -11.96, -0.016, 1200, 0, 0, 0, 0, 0, 0, 0, 0, 5 point.6 = 2, 0, 11.96, -0.016, 1200, 0, 0, 0, 0, 0, 0, 0, 0, 6 static_pitch= 9 static_cg_height= 3.5 gear_system_type = 1 tailwheel_lock = 1 [Views] eyepoint= -0.911, 0, 2.036 [flaps.0] //Trailing Edge Flaps type = 1 span-outboard = 0.5 extending-time = 5 flaps-position.0 = 0 flaps-position.1 = 0, 575 flaps-position.2 = 0, 550 flaps-position.3 = 0, 525 flaps-position.4 = 0, 500 damaging-speed = 575 blowout-speed = 625 system_type = 4 lift_scalar = 1 drag_scalar = 1 pitch_scalar = 1 [electrical] max_battery_voltage = 24 generator_alternator_voltage = 28 max_generator_alternator_amps = 160 electric_always_available = 0 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 [LIGHTS] [Radios] // availiable, standby frequency, has glide slope Audio.1 = 1 Com.1 = 1, 0 Com.2 = 1, 0 Nav.1 = 1, 0, 1 Nav.2 = 1, 0, 0 Adf.1 = 1 Transponder.1 = 1 Marker.1 = 1 [keyboard_response] elevator = 350, 500 aileron = 450, 1000 rudder = 200, 1000 [direction_indicators] direction_indicator.0 = 1, 0 [exits] number_of_exits = 1 exit_rate.0 = 0.4 [EFFECTS] wake = fx_wake water = fx_spray dirt = fx_tchdrt concrete = fx_sparks touchdown = fx_tchdwn, 1 [autopilot] autopilot_available = 1 flight_director_available = 0 default_vertical_speed = 1000 autothrottle_available = 0 autothrottle_arming_required = 0 autothrottle_max_rpm = 90 autothrottle_takeoff_ga = 1 pitch_takeoff_ga = 8 max_pitch_velocity_hi_alt = 1.5 max_pitch_velocity_lo_alt_breakpoint = 20000 max_pitch_velocity_hi_alt_breakpoint = 28000 max_pitch = 10 max_pitch_acceleration = 1 max_pitch_velocity_lo_alt = 2 max_bank= 25 max_bank_acceleration = 1.8 max_bank_velocity = 3 max_throttle_rate = 0.1 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 yaw_damper_gain = 0 [fuel] Center1 = 1.95, 0, 0.1, 10, 0 fuel_type = 1 number_of_tank_selectors = 1 electric_pump=0 [airplane_geometry] wing_area = 100 wing_span = 24 wing_root_chord = 4.16666666666667 wing_dihedral = 5 wing_incidence = 0 wing_twist = 0 oswald_efficiency_factor = 0.878688047088 wing_winglets_flag = 0 wing_sweep = 0 wing_pos_apex_lon = 1.03166666666667 wing_pos_apex_vert = 0 htail_area = 0 htail_span = 13.7 htail_pos_lon = -12 htail_pos_vert = 0 htail_incidence = 0 htail_sweep = 0 vtail_area = 0 vtail_span = 6.4 vtail_sweep = 0 vtail_pos_lon = -10 vtail_pos_vert = 0 elevator_area = 15 aileron_area = 11.5 rudder_area = 7.6 elevator_up_limit = 30 elevator_down_limit = 20 aileron_up_limit = 18 aileron_down_limit = 18 rudder_limit = 35 elevator_trim_limit = 18 spoiler_limit = 0 spoilerons_available = 0 aileron_to_spoileron_gain = 0 min_ailerons_for_spoilerons = 0 min_flaps_for_spoilerons = 0 [Reference Speeds] flaps_up_stall_speed = 35.6 full_flaps_stall_speed = 35.6 cruise_speed = 87 max_indicated_speed = 104 max_mach = 0.1577 [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 [gear_warning_system] gear_warning_available = 1 pct_throttle_limit = 0.1 flap_limit_idle = 0 flap_limit_power = 0 [brakes] toe_brakes_scale = 0.640888698995941 parking_brake = 1 [stall_warning] // 0 = None, 1 = Suction, 2 = Electric. type = 1 [hydraulic_system] electric_pumps = 0 engine_map = 1, 0, 0, 0 normal_pressure = 1000 [attitude_indicators] // 0=None, 1=Vacuum Gyro, 2=Electric Gyro attitude_indicator.0 = 1 [turn_indicators] // 0=None, 1=Electric Gyro, 2=Vacuum Gyro turn_indicator.0 = 1, 0 [direction_indicators] // 0=None, 1=Vac Gyro, 2=Elec Gyro, 3=EM Slave Compass, 4=Slave to other ind direction_indicator.0 = 1, 0 [airspeed_indicators] airspeed_indicator.0 = 1, 0