// AI Helicopter configuration files // by Rob Nieuwenhoven (rjnieuwe@optusnet.com.au) based on the work // of Holger Sandmann (hsandman@sfu.ca) // and Doug Callihan // // Version 1, May 2004 // // for SH-2 SEASPRITE FSDS V2 // by JR Lucariny, http:www.lucariny.sites.uol.com.br // // 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=AI SeaSH2 sim=stemme_as_helicopter_1 model= panel= sound= texture= kb_checklists= prop_anim_ratio=1.20 description=FS2002\/2004 SH-2 SEASPRITE FSDS V2 Model\nBy JRLucariny\nhttp:\/\/lucariny.sites.uol.com.br\nThis Seasprite is a LAMPS-configured SH-2F of HSL-33 "Snakes", whose shore-base is NAS North Island, California. atc_heavy=0 atc_id= atc_airline=Navy atc_flight_number= atc_parking_codes=SH-2 atc_parking_types=MIL_COMBAT [General] performance=Propulsion: 2 T700-GE-401\/401C turboshaft engines\nLength: 52 feet 9 inches (15.9 meters)\nFuselage length: 40 feet 6 inches (12.2 meters)\nHeight: 15 feet (4.5 meters)\nWeight: 9,110 pounds (4100 kg) (empty)\nMaximum Takeoff Weight: 13,500 pounds (6,075 kg)\nRange: 340 nautical miles (391 miles\s 627 km)\nCeiling: 10,000 feet (3048 meters) (at 13,500 pounds (6,075kg))\nSpeed: 150 knots (172.5 mph\s 277.55 kmph)\nCrew: 3\nArmament: 2 Mk 46 or Mk 50 torpedoes\n atc_type=KAMAN atc_model=SH2 //---- misc tweaked parameters [WEIGHT_AND_BALANCE] reference_datum_position=0.000, 0.000, 0.000 empty_weight_CG_position=0.000, 0.000, 0.000 max_number_of_stations=50 station_load.0=0.000000,0.000000,0.000000,0.000000 empty_weight=500 //was 2100.000 (pounds) empty_weight_roll_MOI=9000.000 empty_weight_pitch_MOI=11000.000 empty_weight_yaw_MOI=15000.000 empty_weight_coupled_MOI=0.000 max_gross_weight=1300 //was 2100.000 CG_forward_limit=0.000 CG_aft_limit=1.000 [Reference Speeds] flaps_up_stall_speed=30 full_flaps_stall_speed=27 cruise_speed=110 max_indicated_speed=180.000000 [flight_tuning] cruise_lift_scalar=1.15 // 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=2.5 // was 1.5 pitch_stability=1.0 roll_stability=1.0 yaw_stability=1.5 //was 1.0 elevator_trim_effectiveness=1.0 aileron_trim_effectiveness=1.0 rudder_trim_effectiveness=2.5 // 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 Kaman SH-2, 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=1.000, -14.533, 0.000, -5.500, 3574.803, 0.000, 0.519, 40.320, 0.602, 2.500, 0.609, 3.000, 3.000, 0.000, 0.000, 0.000 point.1=1.000, 3.583, -6.583, -5.500, 3574.803, 1.000, 0.519, 0.000, 0.401, 2.500, 0.746, 3.000, 3.000, 2.000, 0.000, 0.000 point.2=1.000, 3.583, 6.083, -5.500, 3574.803, 2.000, 0.519, 0.000, 0.401, 2.500, 0.746, 3.000, 3.000, 3.000, 0.000, 0.000 //point.0=1.000, -14.333, 0.000, -5.300, 1574.803, 0.000, 0.519, 40.320, 0.602, 2.500, 0.609, 3.000, 3.000, 0.000, 0.000, 0.000 //point.1=1.000, 3.583, -6.083, -5.300, 1574.803, 1.000, 0.519, 0.000, 0.401, 2.500, 0.746, 3.000, 3.000, 2.000, 0.000, 0.000 //point.2=1.000, 3.583, 6.083, -5.300, 1574.803, 2.000, 0.519, 0.000, 0.401, 2.500, 0.746, 3.000, 3.000, 3.000, 0.000, 0.000 //point.3=2.000, -1.083, -22.000, 13.417, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 5.000, 0.000, 0.000 //point.4=2.000, -1.083, 22.000, 13.417, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 6.000, 0.000, 0.000 //point.5=2.000, -26.333, 0.000, 3.500, 787.402, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 9.000, 0.000, 0.000 //point.6=2.000, 10.667, 0.000, 1.500, 787.402, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 4.000, 0.000, 0.000 static_pitch=0.000 static_cg_height=4.000 gear_system_type=0 [keyboard_response] elevator=100.000000,180.000000 //was 0.000000,20480.000000 aileron=200.000000,1000.000000 //was 0.000000,20480.000000 rudder=200.000000,1000.000000 //was 0.000000,20480.000000 [Views] eyepoint=7.561311,1.704499,6.907706 [autopilot] autopilot_available=1 flight_director_available=0 //was 1 default_vertical_speed=500 //was 1800.000000 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 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 //was 3,0 [hydraulic_system] normal_pressure=0.000000 [attitude_indicators] attitude_indicator.0=1 [turn_indicators] turn_indicator.0=1,0 //---- 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=6.000000,0.000000,0.000000 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=200 // 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 [brakes] toe_brakes_scale=1.000000 parking_brake=1 [gear_warning_system] gear_warning_available=0 pct_throttle_limit=0.099976 flap_limit_power=15.996982 flap_limit_idle=0.000000 [stall_warning] type=0
