[fltsim.0] title=hortenIV sim=hortenIV model= panel= sound= texture= kb_checklists= kb_checklists= kb_reference= description=The high-performance Horten Ho IV glider was built for comparative testing of flying wing designs against conventional gliders. The first Horten IV was completed in 1941, and three more were built in 1943. The achievements of the H IV in the air were impressive. ui_manufacturer=Horten ui_type=HoIVa ui_typerole="Glider" ui_createdby=David Rowberry ui_variation=1959 MSU test atc_heavy=0 atc_id= atc_airline= atc_flight_number= [fltsim.1] title=hortenIV_no26 sim=hortenIV model=2 panel= sound= texture=1 kb_checklists= kb_checklists= kb_reference= description=The high-performance Horten Ho IV glider was built for comparative testing of flying wing designs against conventional gliders. The first Horten IV was completed in 1941, and three more were built in 1943. The achievements of the H IV in the air were impressive. ui_manufacturer=Horten ui_type=HoIVa ui_typerole="Glider" ui_createdby=David Rowberry ui_variation=Deutsches Museum atc_heavy=0 atc_id= atc_airline= atc_flight_number= [Electrical] max_battery_voltage=12.0 additional_system=0,0.0,0 avionics_bus=0,0.1,1 avionics=5,0.1,1 pitot_heat=2,10,10 [General] performance=Span - 20.3 m\nWt empty - 246 kg , all up - 330 kg\n Min Sink 0.55m/s @55km/h\nbest glide - 32:1 @73km/h kph\nVNE - 200 km\/h\nStall - 55 km/h\n Category=airplane atc_type= atc_model= [WEIGHT_AND_BALANCE] max_gross_weight = 806.89 empty_weight = 524.33 reference_datum_position = 0.000, 0.000, 0.000 empty_weight_CG_position = -0.80, 0.000, 0.000 max_number_of_stations = 2 station_load.0 =176.000000, -0.500000, 0.000000, 0.000000, Pilot station_load.1 =20.000000, 0.000000, 0.000000, 0.000000, ballast empty_weight_pitch_MOI = 1109.000 empty_weight_roll_MOI = 1289.000 empty_weight_yaw_MOI = 1112.000 empty_weight_coupled_MOI = 0.000 CG_forward_limit= 0.000 CG_aft_limit= 1.000 [flight_tuning] cruise_lift_scalar =1.2 parasite_drag_scalar =0.5 induced_drag_scalar =1.7 elevator_effectiveness =1.0 aileron_effectiveness =1.0 rudder_effectiveness =0.3 pitch_stability =0.3 roll_stability =0.7 yaw_stability =0.8 elevator_trim_effectiveness =1.9 aileron_trim_effectiveness =1.000 rudder_trim_effectiveness =1.000 [GeneralEngineData] engine_type= 1 engine.0= 0.000, 0.000, 0.000 fuel_flow_scalar= 2.000 static_thrust=400 min_throttle_limit=0.000000 [pitot_static] vertical_speed_time_constant = 4 //Increasing this value will cause a more instantaneous reaction in the VSI //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 [contact_points] point.0= 1.000, 1.00, 0.000, -2.42, 1500.000, 0.000, 0.000, 0.000, 0.300, 2.500, 0.75, 1.000, 1.000, 4.000, 0.000, 0.000 point.1= 3.000, -4.55, 0.001, -2.22, 1500.000, 0.000, 0.000, 0.000, 0.200, 0.500, 0.90, 0.000, 0.000, 9.000, 0.000, 0.000 point.2= 3.000, -4.55, -0.001, -2.22, 1500.000, 0.000, 0.000, 0.000, 0.200, 0.500, 0.90, 0.000, 0.000, 9.000, 0.000, 0.000 point.3= 2.000, -10.34, 33.300, 2.080, 900.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 6.000, 0.000, 0.000 point.4= 2.000, -10.34, -33.300, 2.080, 900.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 5.000, 0.000, 0.000 static_pitch= 1.800 static_cg_height= 2.1 gear_system_type=3 [brakes] parking_brake = 1 //Parking brake available toe_brakes_scale = 0.0 //Brake scalar [fuel] electric_pump=1 fuel_type = 2 //Fuel type: 1 = Avgas, 2 = JetA Center1= 0.000, 0.000, 0.000, 1.0, 0.000 number_of_tank_selectors=1 [TurbineEngineData] fuel_flow_gain= 0.022 inlet_area= 1.808 rated_N2_rpm= 29920.000 static_thrust= 400.000 afterburner_available= 0 reverser_available= 0.000 [jet_engine] thrust_scalar=1.000 [hydraulic_system] normal_pressure = 0.0 //PSI [Views] eyepoint = 3.0, 0.0, 3.0 [LIGHTS] //Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing light.0 = 4, 2.7, 0.00, 1.50, fx_vclight, [variometers] variometer.0=54,-116 [Radios] // Radio Type = availiable, standby frequency, has glide slope Audio.1 = 0 Com.1 = 1, 0 Nav.1 = 0, 0, 0 Adf.1 = 0 Transponder.1 = 0 Marker.1 = 0 [keyboard_response] //Breakpoint speeds (knots) on the keyboard increments of control surfaces. //Speed at which the incremenet is reduced to 1/2 and 1/8 respectively. elevator = 160, 360 aileron = 160, 360 rudder = 160, 360 [direction_indicators] //1 Type: 0=None, 1=Vacuum Gyro, 2=Electric Gyro, 3=Electro-Mag Slaved Compass, 4=Slaved to another //2 Indicator number of slaving indicator if Type = 4 direction_indicator.0=0,0 [attitude_indicators] //Type: 0=None, 1=Vacuum Gyro, 2=Electric Gyro attitude_indicator.0 = 0 [turn_indicators] //Type: 0=None, 1=Electric Gyro, 2= Vacuum Gyro turn_indicator.0=0,0 [EFFECTS] wake=fx_wake water=fx_spray dirt=fx_tchdrt concrete=fx_sparks [airplane_geometry] wing_area = 203.400 wing_span = 65.600 wing_root_chord = 5.100 wing_dihedral = 5.000 wing_incidence = 6.000 wing_twist = -2.100 oswald_efficiency_factor= 0.860 wing_winglets_flag = 0 wing_sweep = 17.00 wing_pos_apex_lon = 0.900 wing_pos_apex_vert = 0.000 htail_area = 0.100 htail_span = 0.100 htail_pos_lon = 0.000 htail_pos_vert = 0.000 htail_incidence = 0.000 htail_sweep = 0.000 vtail_area = 0.000 vtail_span = 0.000 vtail_sweep = 0.000 vtail_pos_lon = 0.000 vtail_pos_vert = 0.000 elevator_area = 21.60 aileron_area = 9.240 rudder_area = 4.500 elevator_up_limit = 15.000 elevator_down_limit = 9.000 aileron_up_limit = 16.000 aileron_down_limit = 10.000 rudder_limit = 90.000 elevator_trim_limit = 15.000 spoiler_limit = 70.000 spoilerons_available = 0 aileron_to_spoileron_gain = 0.000 min_ailerons_for_spoilerons = 0.000 min_flaps_for_spoilerons = 0.000 auto_spoiler_available=0 spoiler_extension_time=0.500000 positive_g_limit_flaps_up=5.300000 positive_g_limit_flaps_down=5.300000 negative_g_limit_flaps_up=-2.6500000 negative_g_limit_flaps_down=-2.6500000 [Reference Speeds] flaps_up_stall_speed = 34.600 full_flaps_stall_speed = 34.600 cruise_speed = 45.400 max_indicated_speed = 110.000 //Red line (KIAS) max_mach=0.260010 [autopilot] autopilot_available= 0 flight_director_available= 0 [forcefeedback] ground_bumps_magnitude1=2500 ; 0 - 10000 ground_bumps_angle1=8900 ; 0 - 35999 degrees ground_bumps_intercept1=10.0 ground_bumps_slope1=0.300 ground_bumps_magnitude2=350 ; 0 - 10000 ground_bumps_angle2=9100 ; 0 - 35999 degrees ground_bumps_intercept2=0.075 ground_bumps_slope2=1.0 crash_magnitude1=10000 ; 0 - 10000 crash_direction1=01000 ; 0 - 35999 degrees crash_magnitude2=10000 ; 0 - 10000 crash_direction2=9000 ; 0 - 35999 degrees crash_period2=75000 ; in microseconds crash_duration2=2500000 ; in microseconds [yaw_string] yaw_string_available=1 [stall_warning] type=1 stick_shaker=0 [vacuum_system] max_pressure=5.150000 vacuum_type=0 electric_backup_pressure=0.000000 engine_map=0,0,0,0 [pneumatic_system] max_pressure=0.000000 bleed_air_scalar=0.000000 [deice_system] structural_deice_type=0 [gear_warning_system] gear_warning_available=1 pct_throttle_limit=0.000000 flap_limit_power=0.000000 flap_limit_idle=0.000000 [Flaps.0] type= 1