//********************************************************** Zeppelin R.IV with Mercedes D.III and Benz.IV engines (1917) //********************************************************** // Do not attempt to edit this file with FSedit! - use notepad or wordpad [fltsim.0] title=Zeppelin Staaken R.IV sim=StaakenRIV model= panel= sound= texture= description=Zeppelin Staaken R.IV Riesenflugzeug, 1917, built by Zeppelin Werke in 1917, with composite engines, capable of loads of upto 2000 Kg. atc_airline= atc_flight_number= ui_manufacturer=Zeppelin Werke ui_type=R-IV ui_variation=1917 Splinter Lozenge livery atc_heavy=0 atc_id= [forcefeedback] gear_bump_nose_magnitude=6000 gear_bump_nose_direction=18000 gear_bump_nose_duration=250000 gear_bump_left_magnitude=6000 gear_bump_left_direction=35500 gear_bump_left_duration=250000 gear_bump_right_magnitude=6000 gear_bump_right_direction=00500 gear_bump_right_duration=250000 ground_bumps_magnitude1=3250 ground_bumps_angle1=8900 ground_bumps_intercept1=5.0 ground_bumps_slope1=0.48 ground_bumps_magnitude2=750 ground_bumps_angle2=9100 ground_bumps_intercept2=0.075 ground_bumps_slope2=1.0 crash_magnitude1=10000 crash_direction1=01000 crash_magnitude2=10000 crash_direction2=9000 crash_period2=75000 crash_duration2=2500000 [General] performance=Length: 72 ft 6 in\nWing span: 138 ft 5 in\nWeight: 26,066 lbs\nPower:2x172Hp,Mercedes D.III+4x230Hp,Benz IV.\nMax. speed 135 Kph\nDetails:WW I Bomber\nMax. Load 2 tonnes\n [WEIGHT_AND_BALANCE] reference_datum_position=0.0,0.0,0.0 empty_weight_CG_position=0.0,0.0,0.0 max_number_of_stations=50 station_load.0=0.000000,0.000000,0.000000,0.000000 empty_weight=17600.0 empty_weight_roll_MOI=740000.0 empty_weight_pitch_MOI=450000.0 empty_weight_yaw_MOI=520000.0 empty_weight_coupled_MOI=0 [fuel] LeftMain=0,-22.5,0,293,0 RightMain=0,22.5,0,293,0 fuel_type=1.0 number_of_tank_selectors=1 [airplane_geometry] wing_area=3573 wing_span=138.33 wing_root_chord=12.95 wing_dihedral=0 wing_incidence=6.0 wing_twist=0 oswald_efficiency_factor=0.675 wing_winglets_flag=0 wing_sweep=0.0 wing_pos_apex_lon=0.0 wing_pos_apex_vert=0.0 htail_area=160.0 htail_span=24.0 htail_pos_lon=-48.0 htail_pos_vert=0.0 htail_incidence=0.0 htail_sweep=0.0 vtail_area=120.0 vtail_span=12.489996 vtail_sweep=0.0 vtail_pos_lon=-48.0 vtail_pos_vert=15.0 elevator_area=71.81 aileron_area=130.0 rudder_area=100.0 elevator_up_limit=27.501974 elevator_down_limit=20.626481 aileron_up_limit=17.188734 aileron_down_limit=17.188734 rudder_limit=12.934522 elevator_trim_limit=19.480565 spoiler_limit=59.988681 spoilerons_available=0 aileron_to_spoileron_gain=0.0 min_ailerons_for_spoilerons=0.0 min_flaps_for_spoilerons=0.0 [contact_points] point.0=1,-42.6,0.0,-2.50,1200,0,0.68,10,0.5,2.5,1.0,0.0,0.0,0.0,0.0,0.0 point.1=1.0,0.5,-11.33,-11.6,1574.8,1.0,0.68,0.0,0.6,2.5,0.93,0.0,0.0,2.0,0.0,0.0 point.2=1.0,0.5,11.33,-11.6,1574.8,2.0,0.68,0.0,0.6,2.5,0.93,0.0,0.0,3.0,0.0,0.0 point.3=2.0,-1.667,-69.1667,5.91667,1574.8,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,5.0,0.0,0.0 point.4=2.0,-1.667,69.1667,5.91667,1574.8,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,6.0,0.0,0.0 point.5=2.0,-48.0,0.0,6.583,1574.8,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,9.0,0.0,0.0 point.6=2.0,24.5,0.0,-5.0,1574.8,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,4.0,0.0,0.0 point.7=1.0,25.0,0.0,-9.667,1574.8,0.0,0.632,0.0,1.031,2.5,0.475,0.0,0.0,0.0,0.0,0.0 static_pitch=10.65 static_cg_height=11.5 [GeneralEngineData] engine_type=0 Engine.0=7.250000,-12.916667,1.750000 Engine.1=7.250000,12.916667,1.750000 Engine.2=26.0,0.0,0.0 fuel_flow_scalar=1.0 [piston_engine] ;2x172Hp Mercedes D.III + 4x230Hp Benz.IV=1,264 Hp = mean: 211hp ;2x150.28 + 4x220.6=1182.96 mean displacement=197.16 ;2x4.73 + 4x4.5=18.46 mean compression ratio: 4.57 cylinder_displacement=197.16 ;huge cylinders compression_ratio=4.57 number_of_cylinders=6 max_rated_rpm=1400 max_rated_hp=211 fuel_metering_type=1 cooling_type=0 normalized_starter_torque=0.300000 turbocharged=0 power_scalar=2 max_design_mp=0.0 min_design_mp=0.0 critical_altitude=0 emergency_boost_type=0 emergency_boost_mp_offset=0.0 emergency_boost_gain_offset=0.0 fuel_air_auto_mixture=0 auto_ignition=0 max_rpm_mechanical_efficiency_scalar=1.0 idle_rpm_mechanical_efficiency_scalar=1.0 max_rpm_friction_scalar=1.0 idle_rpm_friction_scalar=1.0 [propeller] gear_reduction_ratio=1.0 ;direct drive fixed_pitch_beta=25.0 ;actual pitch irrelevant - realistic 1917 prop data placed in 25 degree look up table propeller_type=1 propeller_diameter=9.4 ;set to give correct thrust in FS2002 propeller_blades=2 propeller_moi=5 beta_max=25 beta_min=25 min_gov_rpm=400.0 prop_tc=0.100000 low_speed_theory_limit=80.0 prop_sync_available=0 prop_deice_available=0 prop_feathering_available=0 prop_auto_feathering_available=0 min_rpm_for_feather=0.0 beta_feather=0.0 power_absorbed_cf=0.0 defeathering_accumulators_available=0 prop_reverse_available=0 minimum_on_ground_beta=0.0 minimum_reverse_beta=0.0 [Reference Speeds] flaps_up_stall_speed=30.0 full_flaps_stall_speed=24.0 cruise_speed=59.921159 [keyboard_response] elevator=150.0,250.0 aileron=150.0,250.0 rudder=150.0,250.0 [Views] eyepoint=15,-1,2 [autopilot] autopilot_available=0 flight_director_available=0 [direction_indicators] direction_indicator.0=1,0