[fltsim.0] title = OV-1B US Army sim = OV-1B model = panel = sound = texture = panel_alias = sound_alias = kb_checklists = kb_reference = atc_id =14720 atc_id_color = atc_parking_types = atc_parking_code = atc_airline= atc_flight_number= ui_manufacturer = Grumman Aircraft ui_type = OV-1B ui_variation = 73rd Combat Intelligence Company, U.S. Army description = U.S. Army battlefield observation and recon aircraft. Also used for electronic warfare and monitoring by altering the sensors and their configuation. Easily recognized by its bug-eyed canopy, triple fin tail, and top mounted engine nacelles, in addition to the low slung SLAR external pod. Early Mohawks saw action in Viet Nam as armed attack planes, being called the JOV-1A. Also used by Argentina, and formally by Israel, with demo examples briefly flown in West German and French markings. Various civil and non military agencies have also used Mohawks for drug interdiction, survey mapping, and atmospheric studies. visual_damage = 1 prop_anim_ratio = 1.72 [fltsim.1] title = OV-1B USGS sim = OV-1B model =1 panel = sound = texture =usgs panel_alias = sound_alias = kb_checklists = kb_reference = atc_id =N171 atc_id_color = atc_parking_types = atc_parking_code = atc_airline= atc_flight_number= ui_manufacturer = Grumman Aircraft ui_type = OV-1B ui_variation = U.S. Geological Survey description = U.S. Army battlefield observation and recon aircraft. Also used for electronic warfare and monitoring by altering the sensors and their configuation. Easily recognized by its bug-eyed canopy, triple fin tail, and top mounted engine nacelles, in addition to the low slung SLAR external pod. Early Mohawks saw action in Viet Nam as armed attack planes, being called the JOV-1A. Also used by Argentina, and formally by Israel, with demo examples briefly flown in West German and French markings. Various civil and non military agencies have also used Mohawks for drug interdiction, survey mapping, and atmospheric studies. visual_damage = 1 prop_anim_ratio = 1.72 [General] atc_type = atc_model = performance = + Empty Weight: 12147 lbs + Power: 1400 Turbine Shaft HP + Maneuver speed: 289 mph @ 8.0 g + Max speed: 289 mph @ 15000 ft + Max speed at sea-level: 271 mph + Climb rate: 3300 ft/min @ 117 mph Flight Dynamics By: Tim Piglet Conrad Piglet's Peculiar Planes FD Build 18 - 10/16/05 11:37 PM Flight Dynamics Workbook V3.00.09 editable = 1 prop_anim_ratio = 1.72 [pitot_static] vertical_speed_time_constant = 2 [WEIGHT_AND_BALANCE] max_gross_weight = 18109 empty_weight = 11747 reference_datum_position = 0, 0, 0 empty_weight_CG_position = 0.55, 0, 0 CG_forward_limit = 0 CG_aft_limit = 1 max_number_of_stations = 2 station_load.0 = 200, 6, -1.2, 0, Pilot station_load.1 = 200, 6, 1.2, 0, Observer empty_weight_pitch_MOI = 17836 empty_weight_roll_MOI = 20346 empty_weight_yaw_MOI = 35537 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 = 5 Engine.0 = 5.55, -8.67, 0 Engine.1 = 5.55, 8.67, 0 fuel_flow_scalar = 1 min_throttle_limit = -0.25 [TurbineEngineData] fuel_flow_gain = 0.1 inlet_area = 1.2 rated_N2_rpm = 10000 static_thrust = 128 afterburner_available = 0 reverser_available = 0 [turboprop_engine] power_scalar = 1 maximum_torque = 4118 [propeller] thrust_scalar = 1 propeller_type = 0 propeller_diameter = 10.5 propeller_blades = 3 propeller_moi = 36.1 beta_max = 65 beta_min = 15 min_gov_rpm = 7500 prop_tc = 0.01 gear_reduction_ratio = 5.6 fixed_pitch_beta = 25 low_speed_theory_limit = 80 prop_sync_available = 1 prop_deice_available = 1 prop_feathering_available = 1 prop_auto_feathering_available = 1 min_rpm_for_feather = 700 beta_feather = 88.5 power_absorbed_cf = 0.9 defeathering_accumulators_available = 0 prop_reverse_available = 1 minimum_on_ground_beta = 1 minimum_reverse_beta = -14 rotation = 1, 1 [contact_points] max_number_of_points = 7 point.0 = 1, 10.2157, 0, -6.278, 1574, 0, 0.85, 45, 0.545, 1.5, 0.8, 4.8, 4.8, 0, 184, 184 point.1 = 1, -1.6933, -4.2273, -5.6598, 1574, 1, 1.1, 0, 0.642, 2.5, 0.8152, 4.5, 5.2, 2, 184, 184 point.2 = 1, -1.6698, 4.1482, -5.6598, 1574, 2, 1.1, 0, 0.642, 2.5, 0.8152, 5, 6, 3, 184, 184 point.3 = 2, -0.5038, -24.1473, 2.0418, 787, 0, 0, 0, 0, 0, 0, 0, 0, 5 point.4 = 2, -0.7937, 24.1478, 1.9996, 787, 0, 0, 0, 0, 0, 0, 0, 0, 6 point.5 = 2, -23.5674, 0, 0.5491, 787, 0, 0, 0, 0, 0, 0, 0, 0, 9 point.6 = 2, 5.4886, 0, -2.5587, 787, 0, 0, 0, 0, 0, 0, 0, 0, 4 static_pitch= 2.49 static_cg_height= 5.32 gear_system_type = 1 [Views] eyepoint= 8.49, -1.095, 2.44 [flaps.0] //Trailing Edge Flaps type = 1 span-outboard = 0.5 extending-time = 5 flaps-position.0 = 0 flaps-position.1 = 15, 347 flaps-position.2 = 25, 238 flaps-position.3 = 35, 195 flaps-position.4 = 45, 156 damaging-speed = 347 blowout-speed = 391 system_type = 1 lift_scalar = 0 drag_scalar = 0 pitch_scalar = 1 [flaps.1] //Leading Edge Flaps type = 2 span-outboard = 0.5 extending-time = 5 flaps-position.0 = 0 flaps-position.1 = 15 flaps-position.2 = 30 flaps-position.3 = 45 flaps-position.4 = 30 damaging-speed = 347 blowout-speed = 391 system_type = 1 lift_scalar = 1 drag_scalar = 0 pitch_scalar = 0 [flaps.2] //Leading Edge Flaps type = 2 span-outboard = 0.5 extending-time = 5 flaps-position.0 = 0 flaps-position.1 = 4 flaps-position.2 = 5 flaps-position.3 = 6 flaps-position.4 = 45 damaging-speed = 347 blowout-speed = 391 system_type = 1 lift_scalar = 0 drag_scalar = 1 pitch_scalar = 0 [electrical] max_battery_voltage = 24 generator_alternator_voltage = 28 max_generator_alternator_amps = 100 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] //Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit light.0 = 3, 0.22, -24.07, 2.35, fx_navred light.1 = 3, 0.22, 24.07, 2.35, fx_navgre light.2 = 3, -26.95, 0, 1.94, fx_navwhi light.3 = 1, -9.01, 0, -1.79, fx_beacon light.4 = 2, 0.14, -24.07, 2.35, fx_strobe light.5 = 2, 0.14, 24.07, 2.35, fx_strobe light.6 = 1, -23.79, 0, 9.7, fx_beacon light.7 = 4, 8.49, 0.00, 2.44, fx_vclight_deepred light.8 = 8, .17, -8.53, 2.30, fx_smoke_f6, light.9 = 9, .17, 8.53, 2.30, fx_smoke_f6, [Radios] // availiable, standby frequency, has glide slope Audio.1 = 1 Com.1 = 1, 1 Com.2 = 1, 1 Nav.1 = 1, 1, 1 Nav.2 = 1, 1, 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 = 0.8 [EFFECTS] wake = fx_wake water = fx_spray dirt = fx_tchdrt concrete = fx_sparks touchdown = fx_tchdwn, 1 [autopilot] autopilot_available = 1 use_no_default_bank = 1 use_no_default_pitch = 1 flight_director_available = 0 default_vertical_speed = 1000 autothrottle_available = 0 autothrottle_arming_required = 0 autothrottle_takeoff_ga = 1 autothrottle_max_rpm = 90 pitch_takeoff_ga = 8 default_pitch_mode =0 default_bank_mode =0 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 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 = 0, 0, 0.1, 297, 0 External1 = 0, -14.5, -0.39, 150, 0 External2 = 0, 14.5, -0.39, 150, 0 fuel_type = 2 number_of_tank_selectors = 1 electric_pump=1 [airplane_geometry] wing_area = 360 wing_span = 48 wing_root_chord = 7.5 wing_dihedral = 6 wing_incidence = 0 wing_twist = 0 oswald_efficiency_factor = 0.892041532994924 wing_winglets_flag = 0 wing_sweep = 0 wing_pos_apex_lon = 2.425 wing_pos_apex_vert = 0 htail_area = 56.34 htail_span = 15 htail_pos_lon = -23.99 htail_pos_vert = 0 htail_incidence = 0 htail_sweep = 0 vtail_area = 40.5 vtail_span = 8.3 vtail_sweep = 0 vtail_pos_lon = -24.18 vtail_pos_vert = 0 elevator_area = 24.29 aileron_area = 25.73 rudder_area = 36 elevator_up_limit = 30 elevator_down_limit = 20 aileron_up_limit = 18 aileron_down_limit = 15 rudder_limit = 35 elevator_trim_limit = 18 spoiler_limit = 45 spoilerons_available = 0 aileron_to_spoileron_gain = 0 min_ailerons_for_spoilerons = 0 min_flaps_for_spoilerons = 0 [Reference Speeds] flaps_up_stall_speed = 81.7 full_flaps_stall_speed = 69.5 cruise_speed = 217 max_indicated_speed = 326 max_mach = 0.5257 [gear_warning_system] gear_warning_available = 1 pct_throttle_limit = 0.1 flap_limit_idle = 33.75 flap_limit_power = 16.875 [brakes] toe_brakes_scale = 0.85 parking_brake = 1 [stall_warning] // 0 = None, 1 = Suction, 2 = Electric. type = 1 [hydraulic_system] electric_pumps = 0 engine_map = 1, 1, 0, 0 normal_pressure = 3000 [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 [smokesystem] smoke.0 = -2.27, -2.69, -23.51, fx_vapour_f6.fx smoke.1 = -2.27, -2.69, 23.51, fx_vapour_f6.fx