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777-200F.xml
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<!--777-200F yasim
Specs:
2 - GE90-110B1
Typical Cruise = 0.84 Mach / 35000 ft
Max Speed = 0.89 Mach / 35000 ft
Wing span: 64.8 m
Length: 63.7 m
Tail Height: 18.6 m
Diameter : 6.2 m
Wing Area: 427.8 m2
Max Fuel :47,890 US gal
Max TO weight: 766,800 lbs
TO speed : 145 kt
Landing speed : 131 kt
Leading edge MAC = -3.132
Vr 137
V2 147
Datum 92.5 in forward of nose - 2.3495 m
MAC 278.51 in - 7.074154 m
-->
<airplane mass="318300" version="YASIM_VERSION_32">
<!-- Approach configuration -->
<approach speed="132" alt="0.0" aoa="5.0" fuel="0.2" glide-angle="0.0">
<control-setting axis="/controls/engines/engine[0]/throttle-act" value="0.25"/>
<control-setting axis="/controls/engines/engine[1]/throttle-act" value="0.25"/>
<control-setting axis="/controls/flight/flaps" value="1"/>
<control-setting axis="/surface-positions/slats" value="1"/>
<control-setting axis="/controls/gear/gear-down" value="1"/>
<solve-weight idx="0" weight="360"/>
<solve-weight idx="1" weight="42072"/>
</approach>
<!-- Cruise configuration -->
<cruise speed="512" alt="35000" fuel="0.8" glide-angle="0.0">
<control-setting axis="/controls/engines/engine[0]/throttle-act" value="0.95"/>
<control-setting axis="/controls/engines/engine[1]/throttle-act" value="0.95"/>
<control-setting axis="/controls/flight/flaps" value="0.0"/>
<control-setting axis="/controls/flight/elevator-trim" value="0"/>
<control-setting axis="/controls/gear/gear-down" value="0"/>
<solve-weight idx="0" weight="360"/>
<solve-weight idx="1" weight="42072"/>
</cruise>
<cockpit x="22.8" y="0.5" z="0.75"/>
<fuselage ax="25.36" ay="0" az="-0.64" bx="16.231" by="0.00" bz="0.0"
width="6.2" taper="0.0" midpoint="1.0"/>
<fuselage ax="16.231" ay="0" az="0" bx="-20.0" by="0.00" bz="0.0"
width="6.2" taper="1.0" midpoint="0.5"/>
<fuselage ax="-20.0" ay="0" az="0" bx="-37.0" by="0.00" bz="1.2"
width="6.2" taper="0.0" midpoint="0.0"/>
<fuselage ax="4.0" ay="9.8" az="-3" bx="-1.8" by="9.8" bz="-3"
width="3.8" taper="1.0"/>
<fuselage ax="4.0" ay="-9.8" az="-3" bx="-1.8" by="-9.8" bz="-3"
width="3.8" taper="1.0"/>
<wing x="-0.0" y="3.095" z="-1.66" length="31.6" chord="12.8" sweep="32"
taper="0.15" dihedral="7" camber="0.01" incidence="2" twist="-2">
<stall aoa="16" width="6" peak="1.5"/>
<flap0 start="0" end=".56" lift="1.5" drag="1.7"/>
<flap1 start=".64" end=".88" lift="1.5" drag="1.2"/>
<slat start="0" end="1" aoa="2" drag="1"/>
<spoiler start="0.2" end="0.6" lift="0.2" drag="2.0"/>
<control-input axis="/controls/flight/flaps" control="FLAP0"/>
<control-output control="FLAP0" prop="/surface-positions/flap-pos-norm"/>
<control-input axis="/surface-positions/flap-pos-norm" control="SLAT"
src0="0" dst0="0" src1="0.1428" dst1="1.0"/>
<control-output control="SLAT" prop="/surface-positions/slats"/>
<control-speed control="FLAP0" transition-time="78"/>
<control-input axis="/controls/flight/speedbrake" control="SPOILER"/>
<control-output control="SPOILER" prop="/surface-positions/speedbrake-norm"/>
<control-speed control="SPOILER" transition-time="2"/>
<control-input axis="/controls/flight/aileron" control="FLAP1" split="true"/>
<control-input axis="/controls/flight/aileron-trim" control="FLAP1" split="true"/>
<control-output control="FLAP1" side="left" prop="/surface-positions/left-aileron-pos-norm"/>
<control-output control="FLAP1" side="right" prop="/surface-positions/right-aileron-pos-norm"/>
</wing>
<hstab x="-31.0" y="1.5" z="1.0" chord="6.0" length="10.84" taper=".20"
sweep="28" dihedral="7" camber="0.0">
<stall aoa="18" width="5" peak="1.5"/>
<flap0 start="0" end="1" lift="1.4" drag="1.2"/>
<control-input axis="/controls/flight/elevator" control="FLAP0"/>
<control-input axis="/controls/flight/elevator-trim" control="FLAP0"/>
<control-output control="FLAP0" prop="/surface-positions/elevator-trim-tab-pos-norm"/>
</hstab>
<vstab x="-30.0" y="0.00" z="2.7" chord="8.0" length="12.2" taper="0.3"
sweep="33">
<stall aoa="14" width="5" peak="1.5"/>
<flap0 start="0" end="1" lift="1.4" drag="1.2"/>
<control-input axis="/controls/flight/rudder" control="FLAP0" invert="true"/>
<control-input axis="/controls/flight/rudder-trim" control="FLAP0" invert="true"/>
<control-output control="FLAP0" prop="/surface-positions/rudder-pos-norm"
min="1" max="-1"/>
</vstab>
<!-- General Electric GE90-115B
General characteristics
Type: axial flow, twin-shaft, bypass turbofan engine
Length: 287 in (7,290 mm)[14]
Diameter: overall: 135 in (3.429 m);[14] fan: 128 in (3.251 m)
Dry weight: 18,260 lb (8,283 kg)[14]
Components
Compressors: axial: 1 wide chord swept fan, 4 low pressure stages, 9 high pressure stages
Turbines: axial: 6 low pressure stages, 2 high pressure stages
Performance
Maximum thrust: max at sea level: 115,540 lbf (514 kN) ; world record set at 127,900 lbf (568,9 kN) 827 feet above sea level
Overall pressure ratio: 42:1
Thrust-to-weight ratio: approx. 6.3:1
-->
<jet x="1.16" y="9.89" z="-2.995" mass="18260" thrust="115540" spool-time="3"
egt="840" tsfc="0.23 " epr="40" n1-idle="18.5" n1-max="110.5" n2-idle="70" n2-max="107">
<control-input axis="/controls/engines/engine[0]/throttle-act" control="THROTTLE"/>
<control-input axis="/controls/engines/engine[0]/reverser-act" control="REVERSE_THRUST"/>
<control-output control="REVERSE_THRUST" prop="/surface-positions/reverser-norm[0]"/>
<control-speed control="REVERSE_THRUST" transition-time="3"/>
<actionpt x="-2.7" y="9.89" z="-2.995"/>
</jet>
<jet x="1.16" y="-9.89" z="-2.995" mass="18260" thrust="115540" spool-time="3"
egt="840" tsfc="0.23" epr="40" n1-idle="18.5" n1-max="110.5" n2-idle="70" n2-max="107">
<control-input axis="/controls/engines/engine[1]/throttle-act" control="THROTTLE"/>
<control-input axis="/controls/engines/engine[1]/reverser-act" control="REVERSE_THRUST"/>
<control-output control="REVERSE_THRUST" prop="/surface-positions/reverser-norm[1]"/>
<control-speed control="REVERSE_THRUST" transition-time="3"/>
<actionpt x="-2.7" y="-9.89" z="-2.995"/>
</jet>
<!-- nose -->
<gear x="19.28" y="0.00" z="-5.55"
compression="0.7" spring="1.2" damp="1" sfric="1.5" dfric="1.0">
<!-- up to 70 degrees max steering angle with tiller, input is limited to 7 degrees with rudder (see Nasal/ground_steering.nas) -->
<control-input control="STEER" axis="/controls/gear/nosegear-steering-cmd-norm" src0="-1.0" dst0="-1.2217304764" src1="1.0" dst1="1.2217304764" />
<control-output control="STEER" prop="/controls/gear/nosegear-steering-angle-rad" />
<control-input axis="/controls/gear/gear-down" control="EXTEND"/>
<control-output control="EXTEND" prop="/gear/gear[0]/position-norm"/>
<control-speed control="EXTEND" transition-time="19"/>
</gear>
<gear x="-6.39" y="5.6" z="-5.7" compression="0.8" spring="1.0" sfric="1" dfric="0.9">
<control-input axis="/autopilot/autobrake/left-brake-output" control="BRAKE"/>
<control-input axis="/controls/gear/brake-parking" control="BRAKE"/>
<control-input axis="/controls/gear/gear-down" control="EXTEND"/>
<control-output control="EXTEND" prop="/gear/gear[1]/position-norm"/>
<control-speed control="EXTEND" transition-time="20"/>
</gear>
<gear x="-6.39" y="-5.6" z="-5.7" compression="0.8" spring="1.0" sfric="1" dfric="0.9">
<control-input axis="/autopilot/autobrake/right-brake-output" control="BRAKE"/>
<control-input axis="/controls/gear/brake-parking" control="BRAKE"/>
<control-input axis="/controls/gear/gear-down" control="EXTEND"/>
<control-output control="EXTEND" prop="/gear/gear[2]/position-norm"/>
<control-speed control="EXTEND" transition-time="20"/>
</gear>
<!-- aft axle on left main gear -->
<gear x="-7.8" y="5.6" z="-6.22" compression="3.0" spring="1.2" >
<control-input axis="/controls/gear/gear-down" control="EXTEND"/>
<control-output control="EXTEND" prop="/gear/gear[3]/position-norm"/>
<control-speed control="EXTEND" transition-time="20"/>
<!-- 8 degrees main gear steering when nose gear steering above 13 degrees commanded (see Nasal/ground_steering.nas) -->
<control-input control="STEER" axis="/controls/gear/maingear-steering-cmd-norm" src0="-1.0" dst0="-0.1396263402" src1="1.0" dst1="0.1396263402" />
<control-output control="STEER" prop="/controls/gear/maingear-l-steering-angle-rad" />
</gear>
<!-- aft axle on right main gear -->
<gear x="-7.8" y="-5.6" z="-6.22" compression="3.0" spring="1.2">
<control-input axis="/controls/gear/gear-down" control="EXTEND"/>
<control-output control="EXTEND" prop="/gear/gear[4]/position-norm"/>
<control-speed control="EXTEND" transition-time="20"/>
<!-- 8 degrees main gear steering when nose gear steering above 13 degrees commanded (see Nasal/ground_steering.nas) -->
<control-input control="STEER" axis="/controls/gear/maingear-steering-cmd-norm" src0="-1.0" dst0="-0.1396263402" src1="1.0" dst1="0.1396263402" />
<control-output control="STEER" prop="/controls/gear/maingear-r-steering-angle-rad" />
</gear>
<!-- apu -->
<vstab x="0" y="0" z="0" length="0" chord="0">
<flap0 start="0" end="1" lift="0" drag="0"/>
<control-input axis="/controls/APU/running" control="FLAP0"/>
<control-output control="FLAP0" prop="controls/APU/rpm"/>
<control-speed control="FLAP0" transition-time="30"/>
</vstab>
<!--Fuel
Maximum Fuel Capacity Basic - 47,890 U.S. gallons
(181,280 L)
With three optional fuel tanks -
53,515 U.S. gallons (202,570 L)
Source: http://www.boeing.com/commercial/777family/pf/pf_lrproduct.html
-->
<tank x="-4.3" y="5" z="-1.5" jet="true" capacity="70475"/>
<tank x="-4.3" y="0" z="-2.5" jet="true" capacity="180870"/>
<tank x="-4.3" y="-5" z="-1.5" jet="true" capacity="70475"/>
<tank x="-4.3" y="1" z="-8" jet="true" capacity="12600"/>
<tank x="-4.3" y="0" z="-9.5" jet="true" capacity="12600"/>
<tank x="-4.3" y="-1" z="-8" jet="true" capacity="12600"/>
<weight x="22.0" y="0" z="0" mass-prop="/sim/weight[0]/weight-lb"/>
<weight x="-4.3" y="0" z="0" mass-prop="/sim/weight[1]/weight-lb"/>
<ballast x="-30" y="0" z="4" mass="-40000"/>
<thruster x="19.28" y="0.00" z="-5.55" vx="1" vy="0" vz="0" thrust="20000">
<control-input axis="/sim/model/pushback/target-speed-fps" control="THROTTLE"
src0="-1" src1="1" dst0="-1" dst1="1"/>
</thruster>
</airplane>