// AI Helicopter configuration files // by Holger Sandmann (hsandman@sfu.ca) // and Doug Callihan // // Version 1, May 2003 // // for AS316B Alouette III GMax // by Alan Devins, adevins@eircom.net // // based on Stemme motor glider aircraft.cfg // by Al Kaiser, kaiser@va-works.com or http://www.va-works.com/ // // !!!Copyright remains with the original authors!!! [fltsim.0] title=MHAI SA319 HN sim=stemme_as_helicopter_2 model= panel= sound= texture=HN atc_airline=NAVY atc_flight_number= atc_id_color=0xc6eff7ff atc_id=A195 atc_heavy=0 prop_anim_ratio=-1.76 ui_manufacturer=SILENT ui_type=AI Helicopter ui_variation=Hellenic Navy atc_parking_codes=M004 atc_parking_types=RAMP,GATE description=The Alouette III was developed in the late 1950's as an improvement to the Alouette II, with larger cabin and improved equipment, all round performance and greater power.About 1350 were produced in to basic versions at four plants in France, India, Romania and Switzerland.Role Seven Aerospatiale AS316B Alouette III helicopters are in service and serve in a variety of roles with 302 Sqn - Army Support Squadron, based at Baldonnel.Entered Service with Irish Air Corp in November 1963Since 1963, the Alouette III has been the backbone of the Air Corps Helicopter Fleet. They have been employed on a wide variety of mission types, including, Search and Rescue (S.A.R.), Air Ambulance, Security and many more. About 1350 were produced in to basic versions at four plants in France, India, Romania and Switzerland. Role Seven Aerospatiale AS316B Alouette III helicopters are in service and serve in a variety of roles with 302 Sqn - Army Support Squadron, based at Baldonnel. Entered Service with Irish Air Corp in November 1963 Since 1963, the Alouette III has been the backbone of the Air Corps Helicopter Fleet. They have been employed on a wide variety of mission types, including, Search and Rescue (S.A.R.), Air Ambulance, Security and many more. [General] atc_type=Alouette 3 atc_model=ALO3 performance=Cruise speed\95ktsTop Speed\113ktsEngine\1 x 550shp (410KW) Turbomeca Artouste 3B Turbo shaftEndurance\2.5 HRS Service Ceiling\21,300 FTCrew / Passenger No's\1 Pilot, 1 Crew and 5 Passengers (2 Crew for SAR)Range\278 nautical milesRotor Diameter\11mHeight\3mLength\10m //---- misc tweaked parameters [WEIGHT_AND_BALANCE] reference_datum_position=0.000000,0.000000,0.000000 empty_weight_CG_position= 0.000,0.000,-2.000 max_number_of_stations=50 station_load.0=0.000000,0.000000,0.000000,0.000000 max_gross_weight=2300 // (pounds) empty_weight=1300 ;Moments of Inertia empty_weight_pitch_MOI=3000 empty_weight_roll_MOI=4000 empty_weight_yaw_MOI=9000 empty_weight_coupled_MOI=-1000 CG_forward_limit=0.000 CG_aft_limit=1.000 [Reference Speeds] flaps_up_stall_speed=30 full_flaps_stall_speed=27 cruise_speed=80 max_indicated_speed=180.000000 [flight_tuning] cruise_lift_scalar=1.25 // was 1.15 parasite_drag_scalar=0.8 // was 0.8 induced_drag_scalar=0.8 // was 0.8 elevator_effectiveness=1.5 // was 1.0 aileron_effectiveness=1.0 rudder_effectiveness=2.0 // was 1.5 pitch_stability=1.0 roll_stability=1.0 yaw_stability=1.0 elevator_trim_effectiveness=1.0 aileron_trim_effectiveness=1.0 rudder_trim_effectiveness=1.9 // was 1.0 [flaps.0] //Trailing Edge Flaps type=1 // 1 - tail, 2 - lead span-outboard=0.600 // 0.0 .. 1.0 extending-time=4.000 // seconds flaps-position.0=0 // degrees flaps-position.1=0 // degrees flaps-position.2=20 // degrees flaps-position.3=30 // degrees damaging-speed=200 // KIAS blowout-speed=250 // KIAS lift_scalar=1.3 drag_scalar=0.8 pitch_scalar=1.2 system_type=0 //0=Electric, 1=Hydraulic, 2=Pneumatic, 3=Manual, 4=None //---- parameters from Alouette 3, tweaked //0 Class <0=none,1=wheel, 2=scrape, 3=skid> //1 Longitudinal Position (feet) //2 Lateral Position (feet) //3 Vertical Position (feet) //4 Impact Damage Threshold (Feet Per Minute) //5 Brake Map (0=None, 1=Left, 2=Right) //6 Wheel Radius (feet) //7 Steer Angle (degrees) //8 Static Compression (feet) (0 if rigid) //9 Max/Static Compression Ratio //10 Damping Ratio (0=Undamped, 1=Critically Damped) //11 Extension Time (seconds) //12 Retraction Time (seconds) //13 Sound Type //14 Airspeed limit for retraction (KIAS) //15 Airspeed that gear gets damage at (KIAS) [contact_points] point.0 = 1, 6.9514, 0.00, -3.7193, 15574.8, 0, 0.6, 45, 0.500, 0.750, 0.850, 0, 0, 0, 0, 0 point.1 = 1,-2.7904,-4.22, -3.5766, 15574.8, 1, 0.6, 0, 0.500, 0.750, 0.850, 0, 0, 2, 0, 0 point.2 = 1,-2.7904, 4.22, -3.5766, 15574.8, 2, 0.6, 0, 0.500, 0.750, 0.850, 0, 0, 3, 0, 0 //point.0 = 1, 6.9514, 0.00, -3.7193, 15574.8, 0, 0.59, 45, 0.28, 0.5, 0.587, 0, 0, 0, 0, 0 //point.1 = 1,-2.7904,-4.22, -3.5766, 15574.8, 1, 0.6, 0, 0.15, 0.5, 0.728, 0, 0, 2, 0, 0 //point.2 = 1,-2.7904, 4.22, -3.5766, 15574.8, 2, 0.6, 0, 0.15, 0.5, 0.728, 0, 0, 3, 0, 0 //point.3 = 2, -20.9518, 0, -1.5748, 0, 0, 0, 0, 0, 0, 0, 0, 0, 9, 0, 0 //max_number_of_points = 4 static_pitch = 0.1 static_cg_height = 3.7 // was 3.43 [Views] eyepoint=5.6, 2.1, 2.5 [LIGHTS] //Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit light.0 = 3, 7.58, -2.78, -1.09, fx_navred light.1 = 3, 7.58, 2.79, -1.09, fx_navgre light.2 = 1, -11.17, 0, -0.25, fx_beacon light.3 = 2, 3.82, 0, 4.01, fx_strobe light.4 = 4, 7.57, 0, 2.30, fx_vclight [effects] water=fx_spray dirt = fx_tchdrt concrete = fx_tchdrt, 1 touchdown = fx_dustcloud_m, 1 startup=fx_engstrt //touchdown = fx_tchdwn, 1 //landrotorwash = fx_rtr_lnd //waterrotorwash = fx_rtr_wtr [smokesystem] smoke.0 = -2.98, -3.04, 3.93, fx_smoke_yelor smoke.1 = -2.98, -3.04, -3.93, fx_smoke_mgr smoke.2 = 1.76, -21.76, 0, fx_smoke_w //---- parameters from Stemme motor glider, tweaked [fuel] LeftMain=-0.250000,-2.100000,2.500000,6.000000,0.000000 RightMain=-0.250000,2.100000,2.500000,6.000000,0.000000 fuel_type=1.000000 number_of_tank_selectors=1 electric_pump=1 [airplane_geometry] wing_area=400 // was 201.0 wing_span=60 // was 57.0 wing_root_chord=4.916670 wing_dihedral=3.499146 wing_incidence=4.999268 // was 2.999268 wing_twist=-1.994019 oswald_efficiency_factor=.448140 // was 1.064814 wing_winglets_flag=0 wing_sweep=0.000000 wing_pos_apex_lon=1.229000 wing_pos_apex_vert=0.000000 htail_area=16.000000 htail_span=7.916667 htail_pos_lon=-16.083333 htail_pos_vert=0.000000 htail_incidence=0.000000 htail_sweep=0.000000 vtail_area=16.000000 vtail_span=4.560702 vtail_sweep=0.000000 vtail_pos_lon=-14.750000 vtail_pos_vert=4.166667 elevator_area=15.000000 aileron_area=11.740000 rudder_area=6.000000 elevator_up_limit=30.0 // was 25.000447 elevator_down_limit=18.998903 aileron_up_limit=17.996227 aileron_down_limit=13.000035 rudder_limit=20.995472 elevator_trim_limit=10.0 // was 19.497754 spoiler_limit=70 spoilerons_available=1 // was 0 aileron_to_spoileron_gain=0.0005 // was 0 min_ailerons_for_spoilerons=0.005 // was 0 min_flaps_for_spoilerons=0.005 // was 0 [GeneralEngineData] engine_type=0 Engine.0=8.3 Engine.1=8.3 // 'dummy' for tail rotor fuel_flow_scalar=1.00 min_throttle_limit=0.000000 [piston_engine] power_scalar=1.0 //Piston power scalar cylinder_displacement=100.300000 compression_ratio=6.0 number_of_cylinders=6 // was 2 max_rated_rpm=3500 // was 2700 max_rated_hp=100.0 // was 115 fuel_metering_type=1 cooling_type=0 // was 1 normalized_starter_torque=0.3 turbocharged=0 max_design_mp=0.0 min_design_mp=0.0 critical_altitude=0.0 emergency_boost_type=0 emergency_boost_mp_offset=0.000000 emergency_boost_gain_offset=0.000000 fuel_air_auto_mixture=0 auto_ignition=0 max_rpm_mechanical_efficiency_scalar=1.000000 idle_rpm_mechanical_efficiency_scalar=1.000000 max_rpm_friction_scalar=1.000000 idle_rpm_friction_scalar=1.000000 [propeller] thrust_scalar=1.0 // Propeller thrust scalar propeller_type=2 // was 0 propeller_diameter=8.000 // was 5.433000 propeller_blades=2 propeller_moi=20.50000 // was 3.350000 beta_max=29.800000 beta_min=4.000000 // was 17.000000 min_gov_rpm=50.000000 // was 700.000000 prop_tc=0.4 // was 0.004000 gear_reduction_ratio=1.10 // was 1.0 fixed_pitch_beta=0 low_speed_theory_limit=80.000000 prop_sync_available=0 prop_deice_available=0 prop_feathering_available=1 prop_auto_feathering_available=0 min_rpm_for_feather=0 beta_feather=90.0 power_absorbed_cf=0.0 defeathering_accumulators_available=0 // was 1 prop_reverse_available=1 // was 0 minimum_on_ground_beta=2.0 // was 0 minimum_reverse_beta=0.000000 [keyboard_response] elevator=100.000000,180.000000 aileron=200.000000,1000.000000 rudder=200.000000,1000.000000 [autopilot] autopilot_available=1 flight_director_available=0 default_vertical_speed=500.000000 // was 700 autothrottle_available=0 pitch_takeoff_ga=-5.00 // was 8.0 max_pitch=10.000000 max_pitch_acceleration=1.000000 max_pitch_velocity_lo_alt=2.000000 max_pitch_velocity_hi_alt=1.500000 max_pitch_velocity_lo_alt_breakpoint=20000.000000 max_pitch_velocity_hi_alt_breakpoint=28000.000000 max_bank=25.000000 max_bank_acceleration=1.800000 max_bank_velocity=3.000000 max_throttle_rate=0.100000 nav_proportional_control=9.000000 nav_integrator_control=0.250000 nav_derivative_control=0.000000 nav_integrator_boundary=2.500000 nav_derivative_boundary=0.000000 gs_proportional_control=9.520000 gs_integrator_control=0.260000 gs_derivative_control=0.000000 gs_integrator_boundary=0.700000 gs_derivative_boundary=0.000000 yaw_damper_gain=0.000000 [direction_indicators] direction_indicator.0=1,0 [brakes] toe_brakes_scale=1.000000 parking_brake=1 [hydraulic_system] normal_pressure=0.000000 [stall_warning] type=0 [attitude_indicators] attitude_indicator.0=1 [turn_indicators] turn_indicator.0=1,0
