[fltsim.0]
title=Steamship Prinz Heinrich
sim=Steamer
panel=
model=
sound=
texture=
kb_checklists=
kb_reference=
atc_id=
ui_manufacturer=Ship
ui_type=Sh_Prinz Heinrich
ui_variation=
Description=German post and passenger Ship
atc_heavy=0
atc_airline=
atc_flight_number=
[General]
atc_type=CESSNA
atc_model=C208
performance=\n \n \n \n \n \n \n
[WEIGHT_AND_BALANCE]
max_gross_weight= 2800.000
empty_weight= 2000.000
reference_datum_position= 0.000, 0.000, 0.000
empty_weight_CG_position= 0.000, 0.000, 0.000
max_number_of_stations=50
;Moments of Inertia
empty_weight_pitch_MOI=90000
empty_weight_roll_MOI=56000
empty_weight_yaw_MOI=77000
empty_weight_coupled_MOI= 0.000
CG_forward_limit= 0.000
CG_aft_limit= 1.000
station_load.0=0.000000,0.000000,0.000000,0.000000
[Flaps.0]
type= 1
span-outboard= 0.500
extending-time= 5.700
system_type= 0
damaging-speed= 175.000
blowout-speed= 175.000
lift_scalar= 1.000
drag_scalar= 1.000
pitch_scalar= 1.000
flaps-position.0= 0.000, 0.000
flaps-position.1= 10.000, 0.000
flaps-position.2= 20.000, 0.000
flaps-position.3= 30.000, 0.000
[flight_tuning]
cruise_lift_scalar=1.00
parasite_drag_scalar=1.00
induced_drag_scalar=1.00
elevator_effectiveness=1.00
aileron_effectiveness=4.00
rudder_effectiveness=0.1
pitch_stability=1.000
roll_stability=1.000
yaw_stability=1.000
elevator_trim_effectiveness=1.000
aileron_trim_effectiveness=1.000
rudder_trim_effectiveness=1.000
[GeneralEngineData]
engine_type= 5
Engine.0= 0.000, 0.000, 0.500
fuel_flow_scalar= 1.000
min_throttle_limit=-0.25 //Minimum percent throttle. Generally negative for turbine reverser
[propeller]
thrust_scalar=1.000
propeller_type= 0
propeller_diameter= 8.800
propeller_blades= 3
propeller_moi=19.000
beta_max=45.000
beta_min= 15.600
min_gov_rpm= 25520.000
prop_tc= 0.004
gear_reduction_ratio= 17.400
fixed_pitch_beta= 0.000
low_speed_theory_limit= 80.000
prop_sync_available= 0
prop_deice_available= 1
prop_feathering_available= 1
prop_auto_feathering_available= 1
min_rpm_for_feather= 700.000
beta_feather= 88.000
power_absorbed_cf= 0.900
defeathering_accumulators_available= 0
prop_reverse_available= 1.000
minimum_on_ground_beta= 1.000
minimum_reverse_beta= -14.000
[TurbineEngineData]
fuel_flow_gain= 1.000
inlet_area= 1.000
rated_N2_rpm=18000.000
static_thrust=156.000
afterburner_available= 0
[turboprop_engine]
power_scalar=1.000
maximum_torque= 1900.000
max_rpm_mechanical_efficiency_scalar=1.000
idle_rpm_mechanical_efficiency_scalar=1.000
max_rpm_friction_scalar=1.000
idle_rpm_friction_scalar=1.000
[electrical]
;BusType, MaxAmpLoad, MinVoltage BusTypes:0=MainBus,1=AvionicsBus,2=BatteryBus,3=HotBatteryBus,4-7=Generator/AlternatorBus(1-4)
flap_motor=0, 5 , 17.0
gear_motor=0, 5 , 17.0
autopilot=0, 5 , 17.0
avionics_bus=0, 5 , 17.0
avionics=1, 5 , 17.0
pitot_heat=0, 2 , 17.0
additional_system=0, 2 , 17.0
marker_beacon=1, 2 , 17.0
gear_warning=0, 2 , 17.0
fuel_pump=0, 5 , 17.0
starter1=0, 20, 17.0
light_nav=0, 5 , 17.0
light_beacon=0, 5 , 17.0
light_landing=0, 5 , 17.0
light_taxi=0, 5 , 17.0
light_strobe=0, 5 , 17.0
light_panel=0, 5 , 17.0
[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 / Water Rudder Effectiveness (0=Undamped, 1=Critically Damped) / 1.0 = normal
;/11 Extension Time (seconds)
;/12 Retraction Time (seconds)
;/13 Sound Type
;/14 Airspeed limit for retraction (KIAS)
;/15 Airspeed that gear gets damage at (KIAS)
point.0= 4.000, 17.000, -2.60, -1.85, 9600.000, 0.000, 0.000, 0.000, 0.850, 2.500, 0.650, 1.00, 1.00, 0.000, 0.000, 0.000
point.1= 4.000, 17.000, 2.60, -1.85, 9600.000, 0.000, 0.000, 0.000, 0.850, 2.500, 0.650, 0.000, 0.000, 1.000, 0.000, 0.000
point.2= 4.000, -39.000, 5.000, -1.50, 9600.000, 0.000, 0.000, 10.000, 0.950, 2.500, 0.650, 0.000, 0.000, 2.000, 0.000, 0.000
point.3= 4.000, -39.000, -5.000, -1.50, 9600.000, 0.000, 0.000, 10.000, 0.950, 2.500, 0.650, 0.000, 0.000, 3.000, 0.000, 0.000
max_number_of_points=21
static_pitch= 0.000
static_cg_height= 1.000
gear_system_type=1 //Hydraulic
[Views]
//Longitudinal, Lateral, Vertical (feet)
eyepoint= 7.2,0.5, 16.0
[exits]
number_of_exits = 1
exit_rate.0 = 0.4
[gear_warning_system]
gear_warning_available=2 //Amphib
pct_throttle_limit=0.1 //Percent throttle that activates warning
flap_limit_idle=20.1 //Flap angle that activates warning at idle
flap_limit_power=13.0 //Flap angle that activates warning at above idle
[brakes]
parking_brake=1 //Parking brake available
toe_brakes_scale=0.68 //Brake scalar
[hydraulic_system]
normal_pressure=3000.0 //PSI
electric_pumps=0 //no electric pumps
engine_map=1,0,0,0 //pump on Eng1
[Radios]
;/ Radio Type = availiable, standby frequency, has glide slope
Audio.1=1
Com.1=1, 1
Com.2=1, 1
Nav.1=1, 1, 1
Nav.2=1, 1, 0
Adf.1=1
Transponder.1=1
Marker.1=1
[EFFECTS]
wake.1=fx_wake
water.1=fx_spray
[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=100, 180
aileron=200, 1000
rudder=200, 1000
[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=3,0
[attitude_indicators]
;/Type: 0=None, 1=Vacuum Gyro, 2=Electric Gyro
attitude_indicator.0=1
[turn_indicators]
;/Type: 0=None, 1=Electric Gyro, 2=Vacuum Gyro
turn_indicator.0=1,0
//[airspeed_indicators]
airspeed_indicator.0=1.16, -22.0
//[airspeed_indicators]
airspeed_indicator.0=1.16, -22.0
[fuel]
LeftMain= -0.300, -1.100, 2.500, 166.000, 3.600
RightMain= -0.300, 1.100, 2.500, 166.000, 3.600
fuel_type=2 //Fuel type: 1 = Avgas, 2 = JetA
number_of_tank_selectors=1
electric_pump=1
[airplane_geometry]
wing_area= 288.000
wing_span= 46.000
wing_root_chord= 6.400
wing_dihedral= 3.900
wing_incidence= 2.500
wing_twist= -1.700
oswald_efficiency_factor= 0.700
wing_winglets_flag= 0
wing_sweep= 2.960
wing_pos_apex_lon= -12.300
wing_pos_apex_vert= 0.000
htail_area= 39.000
htail_span= 11.700
htail_pos_lon= -27.800
htail_pos_vert= 0.000
htail_incidence= 2.000
htail_sweep= 5.000
vtail_area= 18.000
vtail_span= 4.800
vtail_sweep= 45.000
vtail_pos_lon= -25.700
vtail_pos_vert= 1.000
elevator_area= 16.600
aileron_area=15.000
rudder_area=44.000
elevator_up_limit= 28.000
elevator_down_limit= 21.000
aileron_up_limit= 10.000
aileron_down_limit= 5.000
rudder_limit= 300.000
elevator_trim_limit= 19.500
spoiler_limit= 20.000
spoilerons_available= 1
aileron_to_spoileron_gain= 1.000
min_ailerons_for_spoilerons= 0.000
min_flaps_for_spoilerons= 0.000
spoiler_handle_available=0 //Defaults to True if spoiler limit > 0, else False. Should be False for spoilerons only
[Reference Speeds]
flaps_up_stall_speed=72.000
full_flaps_stall_speed=58.000
cruise_speed=140.000
max_mach=0.60
max_indicated_speed=175 //Red line (KIAS)
[autopilot]
autopilot_available=1
flight_director_available=1
default_vertical_speed=1000.0
autothrottle_available=1
pitch_takeoff_ga=8.0
max_pitch=10.0
max_pitch_acceleration=1.0
max_pitch_velocity_lo_alt=2.0
max_pitch_velocity_hi_alt=1.5
max_pitch_velocity_lo_alt_breakpoint=20000.0
max_pitch_velocity_hi_alt_breakpoint=28000.0
max_bank=25.0
max_bank_acceleration=1.8
max_bank_velocity=3.00
max_throttle_rate=0.10
nav_proportional_control=9.00
nav_integrator_control=0.25
nav_derivative_control=0.00
nav_integrator_boundary=2.50
nav_derivative_boundary=0.00
gs_proportional_control=9.52
gs_integrator_control=0.26
gs_derivative_control=0.00
gs_integrator_boundary=0.70
gs_derivative_boundary=0.00
yaw_damper_gain=0.0
autothrottle_arming_required=0
autothrottle_takeoff_ga=0
autothrottle_max_rpm=90.000000
[forcefeedback]
gear_bump_nose_magnitude=3000 ; 0 - 10000
gear_bump_nose_direction=18000 ; 0 - 35999 degrees
gear_bump_nose_duration=250000 ; in microseconds
gear_bump_left_magnitude=2700 ; 0 - 10000
gear_bump_left_direction=35500 ; 0 - 35999 degrees
gear_bump_left_duration=250000 ; in microseconds
gear_bump_right_magnitude=2700 ; 0 - 10000
gear_bump_right_direction=00500 ; 0 - 35999 degrees
gear_bump_right_duration=250000 ; in microseconds
ground_bumps_magnitude1=1300 ; 0 - 10000
ground_bumps_angle1=08900 ; 0 - 35999 degrees
ground_bumps_intercept1=3.0
ground_bumps_slope1=0.20
ground_bumps_magnitude2=200 ; 0 - 10000
ground_bumps_angle2=09100 ; 0 - 35999 degrees
ground_bumps_intercept2=1.075
ground_bumps_slope2=0.035
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
[stall_warning]
type=2
[LIGHTS]
;type, Z, X, Y, effect
;Light types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing, 6=taxi, 7=recognition, 8=wing, 9=logo
;---internal (bridge)
//Position Order: Z, X, Y (v-h,l-r,o-u)
//light.1 = 4, 68.000, 0.000, 35.000, fx_navred ;night light
;---external
light.2 = 3, 10.8,-10.7, 11.7, fx_navredh ;bridge left
light.3 = 3, 10.8, 10.7, 11.7, fx_navgreh ;bridge right
light.4 = 3, 31.0, 0.0, 29.3, fx_navwhih ;mainmast
light.5 = 3, -61.4, 0.0, 8.4, fx_navwhih ;stern
light.6 = 4, 9.8, 1.1, 13.6, fx_vclighth ;high panel/VC-lighting
light.7 = 4, 9.8, -1.1, 13.6, fx_vclight ;normal panel/VC-lighting
[SMOKESYSTEM]
smoke.1=0,-6.6, 0.0, fx_smoke_tug.fx
