[fltsim.0] title=Grunau_Baby_IIb sim=Grunau_Baby_IIb model= panel= sound= texture= kb_reference=baby_ref kb_checklists=baby_check ui_manufacturer=Grunau ui_type=Baby IIb ui_variation= 1)...German Colors ui_typerole="Glider" ui_createdby"Wolfgang Piper" description=Notes: Advanced training glider Grunau Baby IIb, built about 5000 units all around the world. First design in 1932 and improved 1936 with Schempp-Hirth spoilers. \nThis model is owned by the OSC Wasserkuppe. [fltsim.1] title=Grunau_Baby_IIb Paint1 sim=Grunau_Baby_IIb model= panel= sound= texture=1 kb_reference=baby_ref kb_checklists=baby_check ui_manufacturer=Grunau ui_type=Baby IIb ui_variation=2)...Spanish Colors ui_typerole="Glider" ui_createdby"Wolfgang Piper" description=Notes: Advanced training glider Grunau Baby IIb, built about 5000 units all around the world. First design in 1932 and improved 1936 with Schempp-Hirth spoilers. [fltsim.2] title=Grunau_Baby_IIb Paint2 sim=Grunau_Baby_IIb model= panel= sound= texture=2 kb_reference=baby_ref kb_checklists=baby_check ui_manufacturer=Grunau ui_type=Baby IIb ui_variation=3)...Swiss Colors description=Notes: Advanced training glider Grunau Baby IIb, built about 5000 units all around the world. First design in 1932 and improved 1936 with Schempp-Hirth spoilers. [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 [General] performance=Length: 6.15 m\nWing span: 13.5 m\nWeight: 227 kg max. , 90 kg payload\nGlideratio: 17 \s Vmin 40 km\/h \s Vmax 150\nDetails:\nDesigner: Wolfram Beckert\nDate: 05.02.99\nFlight Dynamics:Wolfgang Piper\n Category=airplane [WEIGHT_AND_BALANCE] reference_datum_position=0.000000,0.000000,0.000000 empty_weight_CG_position=-2.000000,0.000000,0.000000 max_number_of_stations=5 station_load.0="180,2,0,0,Pilot" empty_weight=309.000000 max_gross_weight=501.000000 empty_weight_roll_MOI=500.000000 empty_weight_pitch_MOI=900.000000 empty_weight_yaw_MOI=600.000000 empty_weight_coupled_MOI=0.000000 [airplane_geometry] wing_area=150.000000 wing_span=44.250000 wing_root_chord=3.750000 wing_dihedral=1.000000 wing_incidence=1.000000 wing_twist=-0.999756 oswald_efficiency_factor=1.392217 wing_winglets_flag=0 wing_sweep=0.000000 wing_pos_apex_lon=0.000000 wing_pos_apex_vert=0.000000 htail_area=22.000000 htail_span=9 htail_pos_lon=-13 htail_pos_vert=0.000000 htail_incidence=0.000000 htail_sweep=0.000000 vtail_area=30.000000 vtail_span=3.544998 vtail_sweep=0.000000 vtail_pos_lon=-13 vtail_pos_vert=3.916667 elevator_area=9.460000 aileron_area=11.900000 rudder_area=4.300000 elevator_up_limit=27.501974 elevator_down_limit=20.626481 aileron_up_limit=19.480565 aileron_down_limit=14.896903 rudder_limit=23.491270 elevator_trim_limit=19.480565 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=0.600000 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=0.9 elevator_effectiveness=1.0 aileron_effectiveness=1.2 rudder_effectiveness=1.2 pitch_stability=1.4 roll_stability=1.0 yaw_stability=1.0 elevator_trim_effectiveness=1.3 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 // Lang. Breit. Vert. // Pos. Pos. Pos. // 0 1 2 3 4 5 6 7 8 9 10 11 12 13 14 15 //-------------------------------------------------------------------------------------------------------------------------------- point.0=1, -12.26, 0.5, -0.8, 1574.8, 0, 0.5041, 0, 0.2, 2.5, 0.6, 0, 0, 0, 0, 0 // Gear Tail point.1=1, 0.92, 0.5, -2.0, 1574.8, 2, 0.5041, 0, 0.25, 2.5, 0.7, 0, 0, 3, 0, 0 // Gear Main point.2=2, 0, -20.58, 1.8, 1574.8, 0, 0, 0, 0, 0, 0, 0, 0, 5, 0, 0 // Wing Tip point.3=2, 0, 20.583, 1.8, 1574.8, 0, 0, 0, 0, 0, 0, 0, 0, 6, 0, 0 // Wing Tip point.4=2, -12.26, 0, -0.7, 1574.8, 0, 0, 0, 0, 0, 0, 0, 0, 9, 0, 0 // Tail point.5=2, 4.5, 0, -1.8, 1574.8, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0 // Nose static_pitch=5.998535 static_cg_height=2.333910 //Converted with CPA V.1.05 by Wolfgang Piper //Freitag, 5. September 2003 08:51 //Pilot.View 1.718402 0.000000 1.375075 //gear.center 1.043307 0.000000 -1.853675 //gear.center.1 -12.244061 0.000000 -0.764126 //scrape.side 0.000000 20.803806 1.804462 //scrape.side.1 0.000000 -20.803806 1.804462 //scrape.rear -12.263780 0.000000 -0.728346 [Views] eyepoint=1.72,0.000000,1.37 static_pitch=3.7 static_cg_height=2.0 [GeneralEngineData] engine_type=2 fuel_flow_scalar=1.000000 [Reference Speeds] flaps_up_stall_speed=25.000000 full_flaps_stall_speed=20.000000 cruise_speed=71.087706 max_indicated_speed=152.734375 [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 [fuel] fuel_type=1.000000 [brakes] toe_brakes_scale=1.000031 parking_brake=1 [Flaps.0] type=0 span-outboard=0.500000 extending-time=0.000000 system_type=0 [hydraulic_system] normal_pressure=0.000000 [stall_warning] type=1 stick_shaker=0 [attitude_indicators] attitude_indicator.0=1 [variometers] variometer.0=54,-116 [turn_indicators] turn_indicator.0=1,0 [pitot_static] pitot_heat=0.000000 [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
