//**********************************************************
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