[fltsim.0]
title=Death Glider Z
sim=Death Glider Z
model=
panel=
sound=
texture=
atc_parking_types=RAMP
ui_manufacturer=Ra of the System Lords
ui_type=Class Kah/Jaffa Death Glider
ui_variation=Standard
description=This is a captured Gow'oohl Death Glider from the mothership of Ra during a skurmish on Abidos. This vehicle is highly classified and its handling capabilities are as of yet trully unknow. A covert government group called SGC strongly suggests not taking this craft extra-atmospheric, though it is fully capable of making it to lunar orbit, there exists a 'recall' program in the instrumentation and flight computers, which as of yet are not yet fully declassified.
kb_checklists=
description=
[fltsim.1]
title=Gray Death Glider Z
sim=Death Glider Z
model=
panel=
sound=
texture=1
atc_parking_types=RAMP
ui_manufacturer=Ra of the System Lords
ui_type=Class Kah/Jaffa Death Glider
ui_variation=Gray
description=This is a captured Gow'oohl Death Glider from the mothership of Ra during a skurmish on Abidos. This vehicle is highly classified and its handling capabilities are as of yet trully unknow. A covert government group called SGC strongly suggests not taking this craft extra-atmospheric, though it is fully capable of making it to lunar orbit, there exists a 'recall' program in the instrumentation and flight computers, which as of yet are not yet fully declassified.
kb_checklists=
description=
[General]
atc_type=Death Glider
atc_model=
editable=1
performance=Length: 28feet\nSpan: 41 feet\nWeight: Max. 12,400 lbs.\nPower: Naquida reactor fusion reaction null graviton generator projector\nRange: 4 Earth days of Oxygen, and unknown stats on the naquida reactor fuel lifespan as of yet.\nDesigner: William Ortis\nDate:August 2003\nOriginal designers of the Death Glider are from the creators of the Movie and Series Stargate and StargateSG1\n\n\n
[WEIGHT_AND_BALANCE]
max_gross_weight = 22000.0 // (pounds)
empty_weight = 17000.0 // (pounds)
reference_datum_position = 1.0000, 0.0000, 0.0000 // (feet) distance from FlightSim Reference position: (1/4 chord, centerline, waterline)
empty_weight_CG_position = 0, 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.10 = "100, -42.0, 0.0, 0.0, Baggage1" // Weight(lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.11 = "50, -45.0, 0.0, 0.0, Baggage2" // Weight(lbs), longitudinal, lateral, vertical positions from datum (feet)
;Moments of Inertia
empty_weight_pitch_MOI = 33000000
empty_weight_roll_MOI = 12000000
empty_weight_yaw_MOI = 7500000
empty_weight_coupled_MOI = 150000
reference_datum_position = 0.0000, 0.0000, 0.0000 // (feet) distance from FlightSim Reference position: (1/4 chord, centerline, waterline)
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
[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 = 0.40
parasite_drag_scalar = 1.0
induced_drag_scalar = 1.5
elevator_effectiveness =4.0
aileron_effectiveness = 12.0
rudder_effectiveness = 2.0
pitch_stability = 1.5
roll_stability = 1.0
yaw_stability = 1.0
elevator_trim_effectiveness = 1.0
aileron_trim_effectiveness = 1.0
rudder_trim_effectiveness = 1.0
spoiler_effectiveness = 20.00
[GeneralEngineData]
engine_type = 1 //0=Piston, 1=Jet, 2=None, 3=Helo-Turbine, 4=Rocket, 5=Turboprop
Engine.0 = 0.0, -5.0, 0.0
Engine.1 = 0.0, 5.0, 0.0
fuel_flow_scalar = 2.0 //Scalar for fuel flow efficiency
min_throttle_limit = -0.35 //Minimum percent throttle. Generally negative for turbine reverser
[TurbineEngineData]
fuel_flow_gain = 0.05 //Gain on fuel flow
inlet_area = 6.0 //Square Feet, engine nacelle inlet area
rated_N2_rpm = 29920 //RPM, second stage compressor rated value
static_thrust = 30000 //Lbs, max rated static thrust at Sea Level
afterburner_available = 1 //Afterburner available?
reverser_available = 1 //Thrust reverser available?
[jet_engine]
thrust_scalar = 1.4
//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, 22.00, 0.00, -12.87, 1181.1, 0, 0.6349, 46.8, 0.3000, 2.5, 0.9100, 10.0, 10.0, 0, 260.0, 260.0
point.1=1, -17.25, -15.75, -12.87, 1574.8, 1, 0.6349, 0.0, 0.4798, 2.5, 0.5456, 9.0, 9.0, 2, 260.0, 260.0
point.2=1, -17.25, 15.75, -12.87, 1574.8, 2, 0.6349, 0.0, 0.4798, 2.5, 0.5456, 9.0, 9.0, 3, 260.0, 260.0
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
static_cg_height=14.6
gear_system_type=1 //Hydraulic
[exits]
number_of_exits = 2
exit_rate.0 =0.275 ;Percent per second
exit_rate.1 = 1.40 ;Percent per second
[gear_warning_system]
gear_warning_available = 1 //Normal
pct_throttle_limit = 0.1 //Percent throttle that activates warning
flap_limit_idle = 15.0 //Flap angle that activates warning at idle
flap_limit_power = 30.0 //Flap angle that activates warning at above idle
[brakes]
parking_brake = 1 //Parking brake available
toe_brakes_scale = 3.0 //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 = 5.385, -1.435, 3.012
[LIGHTS]
//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing
light.0 = 3, 10.24, -8.5, -2.05, fx_navgrem ,
light.1 = 3, 10.24, 8.5, -2.05, fx_navgrem ,
light.2 = 3, -9.63, 3.10, 0.55, fx_navwhi ,
light.3 = 1, -7.00, 0.00, -2.90, fx_beaconb ,
light.4 = 2, 6.29, -19.25, -6.08, fx_strobe ,
light.5 = 1, -4.05, 0.00, 3.15, fx_beaconh ,
light.6 = 5, 6.32, -19.25, -6.05, fx_landing ,
light.7 = 5, 6.32, 19.25, -6.05, fx_landing ,
light.8 = 3, -1.00, 0.0, -0.50, fx_navgrem ,
light.9 = 3, -9.63, -3.10, 0.55, fx_navwhi ,
light.10 = 5, 5.00, 4.50, 0.00, fx_landing ,
light.11 = 5, 5.00, -4.50, 0.00, fx_landing ,
light.12 = 1, 1.00, 12.00, -0.50, fx_beaconb ,
light.13 = 1, 1.00, -12.00, -0.50, fx_beaconb ,
light.14 = 2, 6.29, 19.25, -6.08, fx_strobe ,
[flaps.0]
type = 1 // 1 - tail, 2 - lead
span-outboard = 0.8 // 0.0 .. 1.0
extending-time = 6 // seconds
flaps-position.0 = 0 // degrees
flaps-position.1 = 5 // degrees
flaps-position.1 = 10 // degrees
flaps-position.1 = 15 // degrees
flaps-position.2 = 20 // degrees
flaps-position.3 = 40 // degrees
damaging-speed = 1000 // KIAS
blowout-speed = 1200 // KIAS
lift_scalar = 40.0 //1.5
drag_scalar = 18.0
pitch_scalar= 1.0
system_type = 1 //Hydraulic
[flaps.1] //Outboard Leading Edge Slat
type = 2 // 1 - tail, 2 - lead
span-outboard = 0.8 // 0.0 .. 1.0
extending-time = 8 // seconds
flaps-position.0 = 0 //
flaps-position.1 = 0.5 //
flaps-position.4 = 1.0 //
damaging-speed = 1000 // KIAS
blowout-speed = 1200 // KIAS
lift_scalar = 30.0
drag_scalar = 10.0
pitch_scalar= 1.0
system_type = 1 //Hydraulic
[Radios]
// Radio Type = availiable, standby frequency, has glide slope
Audio.1 = 1
Com.1 = 1, 0
Com.2 = 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 = 2
attitude_indicator.1 = 1
[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
touchdown=fx_tchdwn, 1
[fuel]
Center1 = -11.4, 0.0, -1.5, 359.0, 0.0 //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)
LeftMain = -11.3, -10.0, -1.5, 268.5, 0.0 //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)
RightMain = -11.3, 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 = 3500.0 //Square feet
wing_span = 100.0 //Feet
wing_root_chord = 30.9 //Feet
wing_dihedral = 0.0 //Degrees
wing_incidence = 0.0 //Degrees
wing_twist = 0 //Degrees
oswald_efficiency_factor= 1.00 //Measure of lift effeciency of wing
wing_winglets_flag = 1 //Are winglets available?
wing_sweep = 35.0 //Degrees, wing leading edge
wing_pos_apex_lon = 0.0 //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 = 1200.0 //Square feet
htail_span = 100.0 //Feet
htail_pos_lon = -50.0 //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 = 0.0 //Degrees
htail_sweep = 0.0 //Degrees, horizontal tail leading edge
vtail_area = 224.0 //Square feet
vtail_span = 20.0 //Feet, tip to body
vtail_sweep = 35.0 //Degrees, vertical tail leading edge
vtail_pos_lon = 0.0 //Feet, longitudinal distance from reference point, negative going aft
vtail_pos_vert = 0.0 //Feet, vertical distance from reference point, positive going up
elevator_area = 300.0 //Square feet
aileron_area = 300.0 //Square feet
rudder_area = 100.0 //Square feet
elevator_up_limit = 25.0 //Degrees
elevator_down_limit = 35.0 //Degrees
aileron_up_limit = 45.0 //Degrees
aileron_down_limit = 45.0 //Degrees
rudder_limit = 45.0 //Degrees
elevator_trim_limit = 30.0 //Degrees
spoiler_limit = 45.0 //Degrees
spoilerons_available = 0 //Spoilerons Available?
aileron_to_spoileron_gain = 3 //Aileron to spoileron gain
min_ailerons_for_spoilerons = 10 //Degrees
min_flaps_for_spoilerons = 0 //Minimum flap handle position when spoilerons activate
spoiler = 1
[Reference Speeds]
flaps_up_stall_speed = 75.00 //Knots True (KTAS)
full_flaps_stall_speed = 0.5 //Knots True (KTAS)
cruise_speed = 1300 //Knots True (KTAS)
max_mach = 3.00
max_indicated_speed = 1400 //Red line (KIAS)
[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=11.00
nav_integrator_control=0.20
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]
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
