[fltsim.0] title=WA-21 Javelot II sim=WA21 model= panel= sound= texture= kb_reference=WA-21_ref kb_checklists=WA-21_check ui_manufacturer=Wassmer ui_type=WA-21 Javelot II ui_typerole="Glider" ui_createdby"Wolfgang Piper" description="WA-21 'Javelot' II. The French one seat glider F-CCEX, built in 1960. Designer: Wolfgang Piper, March 2006" [electrical] max_battery_voltage=24 avionics_bus=0, 0 , 0 avionics=0, 0 , 0 additional_system=0, 0 , 0 flap_motor=0, 0 , 0 gear_motor=0, 0 , 0 [hydraulic_system] normal_pressure = 0.0 //PSI [General] performance=Span: 15 m\nLength: 7.1 m\nWeight: 210/350 kg\nV max: 200 km\/h\nSink 0.78 m/s at 75 km\/h\nL/D: 27:1 at 85 km/h Category=airplane [WEIGHT_AND_BALANCE] reference_datum_position=0.000000,0.000000,0.000000 empty_weight_CG_position=-1.90,0.000000,0.000000 max_number_of_stations=5 station_load.0="180,2.5,0,0,Pilot" empty_weight=460.000000 empty_weight_roll_MOI=800.000000 empty_weight_pitch_MOI=2200.000000 empty_weight_yaw_MOI=700.000000 empty_weight_coupled_MOI=0.000000 max_gross_weight=770.000000 [airplane_geometry] wing_area=170 wing_span=49 wing_root_chord=3.8 wing_dihedral=1.5000000 wing_incidence=2.5 wing_twist=0.999756 oswald_efficiency_factor=0.8 wing_winglets_flag=0 wing_sweep=0.000000 wing_pos_apex_lon=0.1000000 wing_pos_apex_vert=0.000000 htail_area=22.000000 htail_span=10 htail_pos_lon=-14.000000 htail_pos_vert=-0.5000000 htail_incidence=1.5000000 htail_sweep=0.000000 vtail_area=13.6000000 vtail_span=4.7 vtail_sweep=0.000000 vtail_pos_lon=-13.000000 vtail_pos_vert=3.916667 elevator_area=27 aileron_area=11.700000 rudder_area=8.3 elevator_up_limit=18 elevator_down_limit=15 aileron_up_limit=25 aileron_down_limit=14 rudder_limit=25 elevator_trim_limit=15 spoiler_limit=59.988681 spoilerons_available=0 aileron_to_spoileron_gain=0.000000 min_ailerons_for_spoilerons=0.000000 min_flaps_for_spoilerons=0.000000 auto_spoiler_available=0 spoiler_extension_time=0.500000 positive_g_limit_flaps_up=5.500000 positive_g_limit_flaps_down=5.500000 negative_g_limit_flaps_up=-3.500000 negative_g_limit_flaps_down=-3.500000 [flight_tuning] cruise_lift_scalar=1.2 parasite_drag_scalar=0.7 induced_drag_scalar=1.55 elevator_effectiveness=1.60 aileron_effectiveness=0.7 rudder_effectiveness=1.20 pitch_stability=1.0 roll_stability=0.7 yaw_stability=0.7 elevator_trim_effectiveness=0.9 aileron_trim_effectiveness=1.0 rudder_trim_effectiveness=1.0 [contact_points] //0 Class //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 // Long. Lat. Vert. // Pos. Pos. Pos. // 0 1 2 3 4 5 6 7 8 9 10 11 12 13 14 15 //-------------------------------------------------------------------------------------------------------------------------------- point.0=1, -14.0, 0, -1.12, 1574, 0, 0.5090, 10, 0.3, 2.5, 0.7, 0, 0, 0, 0, 0 // Gear Tail point.1=1, -0.7, 0.4, -3.10, 1574, 1, 0.5090, 0, 0.3, 2.5, 0.90, 0, 0, 2, 0, 0 // Gear Main point.2=2, 0.00, -24.7, 0.80, 1574, 0, 0, 0, 0, 0, 0, 0, 0, 5, 0, 0 // Wing Tip point.3=2, 0.00, 24.7 , 0.80, 1574, 0, 0, 0, 0, 0, 0, 0, 0, 6, 0, 0 // Wing Tip point.4=2, -14, 0, -1.05, 1687 ,0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0 // Tail point.5=2, 6 0, -2.62, 1574, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0 // Nose point.6=2, 1.7 0, -2.87, 1574, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0 // Nose //Converted with CPA V.1.05 by Wolfgang Piper pilot.view 2.245410 0.000000 0.68 static_pitch=5 static_cg_height=3.1 [Views] eyepoint=2.46,0,0.68 [Reference Speeds] flaps_up_stall_speed=32.000000 full_flaps_stall_speed=30.000000 cruise_speed=43 max_indicated_speed=150.000000 max_mach=0.399902 [keyboard_response] elevator=150.000000,250.000000 aileron=150.000000,250.000000 rudder=150.000000,250.000000 [autopilot] autopilot_available=0 flight_director_available=0 [direction_indicators] direction_indicator.0=0,0 [brakes] toe_brakes_scale=0.5 parking_brake=0 [hydraulic_system] normal_pressure=0.000000 [stall_warning] type=1 stick_shaker=0 [attitude_indicators] attitude_indicator.0=1 [turn_indicators] turn_indicator.0=1,0 [exits] number_of_exits=3 exit_rate.0=0.4 exit_rate.1=0.4 exit_rate.2=0.8 //[variometers] //variometer.0=54,-116 [fuel] fuel_type=1.000000 [Flaps.0] type=1 span-outboard=0.500000 extending-time=0.000000 system_type=0 [GeneralEngineData] engine_type=2 fuel_flow_scalar=1.000000 [pitot_static] pitot_heat=1.000000 [vacuum_system] max_pressure=0.000000 vacuum_type=0 electric_backup_pressure=0.000000 engine_map=1,1,1,1 [pneumatic_system] max_pressure=0.000000 bleed_air_scalar=0.000000 [deice_system] structural_deice_type=0
