[fltsim.0]
title=Seruphum
sim=Seruphum
model=
panel=
sound=
texture=
panel_alias = beech_king_air_350\panel
sound_alias = beech_king_air_350\sound
kb_checklists=
kb_reference=
atc_id=NTECJ
ui_manufacturer=Seruphum Aerospace
description=This is the prototype delta winged Seruphum aircraft. It is a multi task, multi platformed concept designed for STOL landings in remote area's and would range in use from Med Evac, Cargo, Commuter to Executive high end markets. This version of the Seruphum is powered by the Pratt and Whitney turbo props. Other versions include the GE turbine powerplants. The Seruphum primary hull, which is a lifting body to allow for a maximum area rectangular cross section is also a lifting body shape to allow for smaller wings. The Seruphum carries 12 people including the crew and features an additional loading ramp at the rear of the plane.
[fltsim.1]
title=Black Seruphum
sim=Seruphum
model=
panel=
sound=
texture=1
kb_checklists=
kb_reference=
atc_id=
ui_manufacturer=Seruphum Aerospace
ui_type=Black Seruphum
ui_variation=Black
description=This is the prototype delta winged Seruphum aircraft. It is a multi task, multi platformed concept designed for STOL landings in remote area's and would range in use from Med Evac, Cargo, Commuter to Executive high end markets. This version of the Seruphum is powered by the Pratt and Whitney turbo props. Other versions include the GE turbine powerplants. The Seruphum primary hull, which is a lifting body to allow for a maximum area rectangular cross section is also a lifting body shape to allow for smaller wings. The Seruphum carries 12 people including the crew and features an additional loading ramp at the rear of the plane.
[fltsim.2]
title=Silver Seruphum
sim=Seruphum
model=
panel=
sound=
texture=2
kb_checklists=
kb_reference=
atc_id=
ui_manufacturer=Seruphum Aerospace
ui_type=Silver Seruphum
ui_variation=Striped
description=This is the prototype delta winged Seruphum aircraft. It is a multi task, multi platformed concept designed for STOL landings in remote area's and would range in use from Med Evac, Cargo, Commuter to Executive high end markets. This version of the Seruphum is powered by the Pratt and Whitney turbo props. Other versions include the GE turbine powerplants. The Seruphum primary hull, which is a lifting body to allow for a maximum area rectangular cross section is also a lifting body shape to allow for smaller wings. The Seruphum carries 12 people including the crew and features an additional loading ramp at the rear of the plane.
[fltsim.3]
title=AirEvac Seruphum
sim=Seruphum
model=
panel=
sound=
texture=3
kb_checklists=
kb_reference=
atc_id=
ui_manufacturer=Seruphum Aerospace
ui_type=AirEvac Seruphum
ui_variation=AirEvac
description=This is the prototype delta winged Seruphum aircraft. It is a multi task, multi platformed concept designed for STOL landings in remote area's and would range in use from Med Evac, Cargo, Commuter to Executive high end markets. This version of the Seruphum is powered by the Pratt and Whitney turbo props. Other versions include the GE turbine powerplants. The Seruphum primary hull, which is a lifting body to allow for a maximum area rectangular cross section is also a lifting body shape to allow for smaller wings. The Seruphum carries 12 people including the crew and features an additional loading ramp at the rear of the plane.
[fltsim.4]
title=Blue Striped Seruphum
sim=Seruphum
model=
panel=
sound=
texture=4
kb_checklists=
kb_reference=
atc_id=
ui_manufacturer=Seruphum Aerospace
ui_type=Blue Stripes
ui_variation=AirEvac
description=This is the prototype delta winged Seruphum aircraft. It is a multi task, multi platformed concept designed for STOL landings in remote area's and would range in use from Med Evac, Cargo, Commuter to Executive high end markets. This version of the Seruphum is powered by the Pratt and Whitney turbo props. Other versions include the GE turbine powerplants. The Seruphum primary hull, which is a lifting body to allow for a maximum area rectangular cross section is also a lifting body shape to allow for smaller wings. The Seruphum carries 12 people including the crew and features an additional loading ramp at the rear of the plane.
[fltsim.5]
title=AirForce Troop Transport
sim=Seruphum
model=
panel=
sound=
texture=5
kb_checklists=
kb_reference=
atc_id=
ui_manufacturer=Seruphum Aerospace
ui_type=AirForce Troop Transport
ui_variation=Troop Transport
description=This is the prototype delta winged Seruphum aircraft. It is a multi task, multi platformed concept designed for STOL landings in remote area's and would range in use from Med Evac, Cargo, Commuter to Executive high end markets. This version of the Seruphum is powered by the Pratt and Whitney turbo props. Other versions include the GE turbine powerplants. The Seruphum primary hull, which is a lifting body to allow for a maximum area rectangular cross section is also a lifting body shape to allow for smaller wings. The Seruphum carries 12 people including the crew and features an additional loading ramp at the rear of the plane.
[fltsim.6]
title=UPS Seruphum
sim=Seruphum
model=
panel=
sound=
texture=6
kb_checklists=
kb_reference=
atc_id=
ui_manufacturer=Seruphum Aerospace
ui_type=UPS Seruphum
ui_variation=UPS Seruphum
description=This is the prototype delta winged Seruphum aircraft. It is a multi task, multi platformed concept designed for STOL landings in remote area's and would range in use from Med Evac, Cargo, Commuter to Executive high end markets. This version of the Seruphum is powered by the Pratt and Whitney turbo props. Other versions include the GE turbine powerplants. The Seruphum primary hull, which is a lifting body to allow for a maximum area rectangular cross section is also a lifting body shape to allow for smaller wings. The Seruphum carries 12 people including the crew and features an additional loading ramp at the rear of the plane.
ui_type=
ui_variation=
description=Enter your description here.
[General]
atc_type=Seruphum
atc_model=
editable=1
performance=Enter your performance information here.
[WEIGHT_AND_BALANCE]
max_gross_weight = 18000.0 // (pounds)
empty_weight = 4800.0 // (pounds)
reference_datum_position = 34.5, 0, 0 // (feet) distance from FlightSim Reference position, which is: (1/4 chord, centerline, waterline)
empty_weight_CG_position = -30.79, 0, 0 // (feet) longitudinal, lateral, vertical distance from specified datum
max_number_of_stations = 50
station_load.0 = 170, -17.0, -1.2, 0.0 //Pilot Weight(lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.1 = 170, -17.0, 1.2, 0.0 //Co-Pilot Weight(lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.2 = 170, -22.5, -1.2, 0.0 //Pssngr 1 Weight(lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.3 = 170, -22.5, 1.2, 0.0 //Pssngr 2 Weight(lbs), longitudinal, lateral, vertical positions from datum (feet)
\
;Moments of Inertia
empty_weight_pitch_MOI = 600000
empty_weight_roll_MOI = 45000
empty_weight_yaw_MOI = 70000
empty_weight_coupled_MOI = 0.0
[electrical]
max_battery_voltage = 12.0
generator_alternator_voltage = 13.8
max_generator_alternator_amps = 40.0
;BusType, MaxAmpLoad, MinVoltage BusTypes:0=MainBus,1=AvionicsBus,2=BatteryBus,3=HotBatteryBus,4-7=Generator/AlternatorBus(1-4)
avionics_bus = 0, 5 , 9.5
avionics = 1, 5 , 9.5
additional_system = 0, 2 , 9.5
marker_beacon = 1, 2 , 9.0
fuel_pump = 0, 5 , 9.0
[flight_tuning]
cruise_lift_scalar = 1.3
parasite_drag_scalar = 1.0
induced_drag_scalar = 1.4
elevator_effectiveness = 1.6
aileron_effectiveness = 1.0
rudder_effectiveness = 1.0
pitch_stability = 1.4
roll_stability = 1.0
yaw_stability = 1.0
elevator_trim_effectiveness = 1.0
aileron_trim_effectiveness = 1.0
rudder_trim_effectiveness = 1.0
[GeneralEngineData]
engine_type = 1 //0=Piston, 1=Jet, 2=None, 3=Helo-Turbine, 4=Rocket, 5=Turboprop
Engine.0 = -42.8, -4.8, 0.8 //(feet) longitudinal, lateral, vertical distance from reference datum
Engine.1 = -42.8, 4.8, 0.8 //(feet) longitudinal, lateral, vertical distance from reference datum
fuel_flow_scalar = 1.0 //Scalar for fuel flow efficiency
min_throttle_limit = -0.25 //Minimum percent throttle. Generally negative for turbine reverser
[TurbineEngineData]
fuel_flow_gain = 0.0025 //Gain on fuel flow
inlet_area = 4.2895 //Square Feet, engine nacelle inlet area
rated_N2_rpm = 29920 //RPM, second stage compressor rated value
static_thrust = 3500 //Lbs, max rated static thrust at Sea Level
afterburner_available = 0 //Afterburner available?
reverser_available = 1 //Thrust reverser available?
[jet_engine]
thrust_scalar = 1.0
//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, -11.17, 0.00, -8.24, 1181.1, 0, 0.5349, 46.8, 0.6197, 2.5, 2.8878, 4.3, 4.3, 0, 0.0, 0.0
point.1=1, -47.75, -10.85, -8.75, 1574.8, 1, 0.6349, 0.0, 0.6798, 2.5, 2.8456, 4.1, 4.1, 2, 0.0, 0.0
point.2=1, -47.75, 10.85, -8.75, 1574.8, 2, 0.6349, 0.0, 0.6798, 2.5, 2.8456, 4.0, 4.0, 3, 0.0, 0.0
point.3=2, -37.83, -23.92, -3.00, 787.4, 0, 0.0000, 0.0, 0.0000, 0.0, 0.0000, 0.0, 0.0, 5, 0.0, 0.0
point.4=2, -37.83, 23.92, -3.00, 787.4, 0, 0.0000, 0.0, 0.0000, 0.0, 0.0000, 0.0, 0.0, 6, 0.0, 0.0
point.5=2, -57.17, 0.00, 0.00, 787.4, 0, 0.0000, 0.0, 0.0000, 0.0, 0.0000, 0.0, 0.0, 9, 0.0, 0.0
point.6=2, -11.47, 0.00, -1.50, 787.4, 0, 0.0000, 0.0, 0.0000, 0.0, 0.0000, 0.0, 0.0, 4, 0.0, 0.0
static_pitch = 0.75
static_cg_height = 8.41
gear_system_type=1 //Hydraulic
[gear_warning_system]
gear_warning_available = 1 //Normal
pct_throttle_limit = 0.1 //Percent throttle that activates warning
flap_limit_idle = 0.0 //Flap angle that activates warning at idle
flap_limit_power = 16.0 //Flap angle that activates warning at above idle
[brakes]
parking_brake = 1 //Parking brake available
toe_brakes_scale = 1.0 //Brake scalar
[hydraulic_system]
normal_pressure = 3000.0 //PSI
electric_pumps = 0 //no electric pumps
engine_map = 1,1,0,0 //pumps on Eng1,2
[Views]
eyepoint = -11.41, -1.31, 2.34
[LIGHTS]
//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing
light.0 = 3, -59.00, -24.2, 7.34, fx_navredm ,
light.1 = 3, -59.00, 24.98, 7.34, fx_navgrem ,
light.2 = 3, -61.50, 5.00, 2.57, fx_navwhi ,
light.3 = 1, -37.00, 0.00, -1.99, fx_beaconb ,
light.4 = 2, -36.97, 0.00, -1.92, fx_strobe ,
light.5 = 4, -22.00, 0.00, 3.00, fx_vclighth,
light.6 = 4, -27.00, 0.00, 3.00, fx_vclighth,
light.7 = 2, -59.10, -24.2, 7.34, fx_strobe ,
light.8 = 2, -59.10, 24.98, 7.34, fx_strobe ,
light.9 = 5, -37.7, 0.00, 3.00, fx_vclighth ,
light.10 = 5, -60.7, 0.00, 3.00, fx_vclighth ,
light.11 = 4, -10.00, 0.00, 1.80, fx_vclighth,
light.12 = 4, -20.00, 1.00, 3.00, fx_vclighth,
light.13 = 5, -60.7, 0.00, -6.00, fx_vclighth ,
light.14 = 4, -20.00, -9.00, -6.00, fx_vclighth,
light.15 = 3, -61.50, -5.00, 2.57, fx_navwhi ,
[flaps.0]
type = 1 // 1 - tail, 2 - lead
span-outboard = 0.8 // 0.0 .. 1.0
extending-time = 5 // seconds
flaps-position.0 = 0 // degrees
flaps-position.1 = 8 // degrees
flaps-position.2 = 20 // degrees
flaps-position.3 = 40 // degrees
damaging-speed = 250 // KIAS
blowout-speed = 300 // KIAS
[Radios]
// Radio Type = availiable, standby frequency, has glide slope
Audio.1 = 1
Com.1 = 1, 0
Nav.1 = 1, 0, 1
Nav.2 = 1, 0, 0
Adf.1 = 1
Transponder.1 = 1
Marker.1 = 1
[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 = 150, 250
aileron = 150, 250
rudder = 150, 250
[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
[exits]
number_of_exits = 2
exit_rate.0 = 0.18 ;Percent per second
exit_rate.1 = 0.18 ;Percent per second
[turn_indicators]
//Type: 0=None, 1=Electric Gyro, 2= Vacuum Gyro
turn_indicator.0=1,0
[EFFECTS]
wake=fx_wake
water=fx_spray
dirt=fx_tchdrt
concrete=fx_sparks
touchdown=fx_tchdwn, 1
[fuel]
Center1 = -41.4, 0.0, -1.5, 359.0, 0.0 //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)
LeftMain = -36.3, -10.0, -1.5, 268.5, 0.0 //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)
RightMain = -36.3, 10.0, -1.5, 268.5, 0.0 //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)
fuel_type = 2 //Fuel type: 1 = Avgas, 2 = JetA
number_of_tank_selectors = 1
electric_pump=1
[airplane_geometry]
wing_area = 412.0 //Square feet
wing_span = 48.8 //Feet
wing_root_chord = 36.3 //Feet
wing_dihedral = -2.5 //Degrees
wing_incidence = 0.5 //Degrees
wing_twist = -1.5 //Degrees
oswald_efficiency_factor= 0.8 //Measure of lift effeciency of wing
wing_winglets_flag = 1 //Are winglets available?
wing_sweep = 60.0 //Degrees, wing leading edge
wing_pos_apex_lon = -28.0 //Feet, longitudinal distance from reference point, negative going aft
wing_pos_apex_vert = 0.0 //Feet, vertical distance from reference point, positive going up
htail_area = 67.0 //Square feet
htail_span = 17.2 //Feet
htail_pos_lon = -59.1 //Feet, longitudinal distance from reference point, negative going aft
htail_pos_vert = 0.0 //Feet, vertical distance from reference point, positive going up
htail_incidence = 2.0 //Degrees
htail_sweep = 25.0 //Degrees, horizontal tail leading edge
vtail_area = 42.0 //Square feet
vtail_span = 7.4 //Feet, tip to body
vtail_sweep = 30.0 //Degrees, vertical tail leading edge
vtail_pos_lon = -55.0 //Feet, longitudinal distance from reference point, negative going aft
vtail_pos_vert = 4.1 //Feet, vertical distance from reference point, positive going up
elevator_area = 60.0 //Square feet
aileron_area = 13.5 //Square feet
rudder_area = 12.3 //Square feet
elevator_up_limit = 42.0 //Degrees
elevator_down_limit = 28.5 //Degrees
aileron_up_limit = 18.0 //Degrees
aileron_down_limit = 18.0 //Degrees
rudder_limit = 30.0 //Degrees
elevator_trim_limit = 15.0 //Degrees
spoiler_limit = 40.0 //Degrees
spoilerons_available = 1 //Spoilerons Available?
aileron_to_spoileron_gain = 4.6 //Aileron to spoileron gain
min_ailerons_for_spoilerons = 5 //Degrees
min_flaps_for_spoilerons= 0.0 //Minimum flap handle position when spoilerons activate
[Reference Speeds]
flaps_up_stall_speed = 36.0 //Knots True (KTAS)
full_flaps_stall_speed = 36.0 //Knots True (KTAS)
cruise_speed = 480.0 //Knots True (KTAS)
max_mach = 0.80
max_indicated_speed = 480.000000
[autopilot]
autopilot_available= 1
flight_director_available= 1
default_vertical_speed= 1800.0
autothrottle_available= 1
autothrottle_arming_required= 0
autothrottle_max_rpm = 90
autothrottle_takeoff_ga= 0
pitch_takeoff_ga = 8
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 = 1.0
[forcefeedback]
stick_shaker_magnitude=5000 ; 0 - 10000
stick_shaker_direction=0 ; 0 - 35999 degrees
stick_shaker_period=111111 ; in microseconds
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=9000 ; 0 - 35999 degrees
gear_bump_left_duration=250000 ; in microseconds
gear_bump_right_magnitude=2700 ; 0 - 10000
gear_bump_right_direction=27000 ; 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=1
[fltsim.4]
title=Seruphum Glass Panel
sim=Seruphum
model=
panel=Glass Panel
sound=
texture=
panel_alias=lear45\panel
sound_alias=lear45\sound
kb_checklists=
kb_reference=
atc_id=NTECJ
ui_manufacturer=Seruphum Aerospace
description=Full Digital Instrumentation Version Glass panel
ui_variation=Glass Panel
