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F-18old-yasim.xml
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F-18old-yasim.xml
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<?xml version="1.0" encoding="UTF-8"?>
<!-- F-18C/D Hornet
Power Plant Two F404-GE-402 afterburning engines, each in the 18,000 pound thrust class,
which results in a combat thrust-to-weight ratio greater than 1-to-1.
Depending on the mission and loading, combat radius is greater than 500 nautical miles.
Accommodations - The F/A-18C and F/A-18E are single seat aircraft.
- The D and F models are flown by two crew members.
- The aft seat in the D and F may be configured with a stick and throttle for the training environment (or without when crewed with a Weapons System Officer).
Performance - F/A-18C maximum speed at level flight in altitudes of 36,089 ft. Mach 1.7
Armament - F/A-18C/D can carry up to 13,700 pounds of external ordnance.
- Weapon stations include: two wingtip stations for Sidewinders; two outboard wing stations for air-to-air or air-to-ground weapons; two inboard wing stations for fuel tanks, air-to-air, or air-to-ground weapons; two nacelle fuselage stations for AMRAAMs, Sparrows, or sensor pods; and one centerline station for fuel or air-to-ground weapons.
M61 Vulcan 6-barrel rotary cannon with 520 rounds of 20mm ammunition is internally mounted in the nose
AIM-9 Sidewinder
AIM-7F Sparrow
AIM-120 AMRAAM
AGM-65E Maverick
AGM-84 Harpoon
AGM-88A HARM
MK82
10 CBU-87
10 CBU-89
GBU-12
GBU-24
JDAM
B-57 or B-61 Nuclear bomb
-->
<airplane mass="23000">
<!--
<airplane mass="23000" version="YASIM_VERSION_CURRENT">
-->
<!-- Approach configuration -->
<approach speed="134" aoa="8" fuel="0.3">
<control-setting axis="/controls/engines/engine[0]/throttle" value="0.2"/>
<control-setting axis="/controls/engines/engine[1]/throttle" value="0.2"/>
<control-setting axis="/controls/flight/flaps" value="1.0"/>
<control-setting axis="/controls/flight/slats" value="0.5"/>
<control-setting axis="/controls/gear/gear-down" value="1"/>
</approach>
<!-- Cruise configuration -->
<cruise speed="580" alt="35000" fuel="1.0">
<control-setting axis="/controls/engines/engine[0]/throttle" value="0.76"/>
<control-setting axis="/controls/engines/engine[1]/throttle" value="0.76"/>
<control-setting axis="/controls/flight/flaps" value="0.0"/>
<control-setting axis="/controls/gear/gear-down" value="0"/>
</cruise>
<!-- pilot eyepoint -->
<cockpit x="3.5" y="0.0" z="1.4"/>
<!-- Cockpit -->
<fuselage ax="6" ay="0" az="0.1" bx="0" by="0" bz="0.8"
width="1.3" taper= "0.1" midpoint= "0.6" />
<!-- Nose cone -->
<fuselage ax="9" ay="0" az="-0.15" bx="6.00" by="0" bz="-0.19"
width="0.6" taper="0.05" midpoint="1.00"/>
<!-- Tail cone -->
<fuselage ax="-5.7" ay="0" az="-0.1" bx="-6.7" by="0" bz="-0.1"
width="0.6" taper="0.05" midpoint="0"/>
<!-- front fuselage -->
<fuselage ax="7" ay="0" az="-0.2" bx="-0.7" by="0" bz="0.5" width="1.3" taper= "0.3" midpoint= "0.6" />
<!-- rear fuselage -->
<fuselage ax="7" ay="0" az="-0.2" bx="-5.7" by="0" bz="0.1" width="1.3" taper= "0.3" midpoint= "0.6" cx="2" cz="2" cy="2"/>
<!-- Engines -->
<fuselage ax="0" ay="0.8" az="-0.1" bx="-7.4" by="0.5" bz="-0.1" width="0.8" taper= "1.0" midpoint= "0.6" idrag="0.7" />
<fuselage ax="0" ay="-0.8" az="-0.1" bx="-7.4" by="-0.5" bz="-0.1" width="0.8" taper= "1.0" midpoint= "0.6" idrag="0.5" />
<wing x="-2.0" y="1.283" z="0.3"
taper="0.414"
incidence="1.3"
twist="-2.0"
idrag="0.5"
length="4.8"
chord="4.1"
sweep="12.5"
dihedral="-2">
<stall aoa="21" width="8" peak="1.3"/>
<flap0 start="0.0" end="0.47" lift="1.5" drag="1.3"/>
<flap1 start="0.47" end="0.813" lift="1.3" drag="1.1"/>
<slat aoa="4" start="0.0" end="0.813" lift="1.5" drag="1.5"/>
<control-input axis="/controls/flight/flaps" control="FLAP0"/>
<control-input axis="/controls/flight/aileron" control="FLAP1" split="true"/>
<control-input axis="/controls/flight/aileron-trim" control="FLAP1" split="true"/>
<control-input axis="/controls/flight/slats" control="FLAP0"/>
<control-output control="FLAP0" prop="/surface-positions/flap-pos-norm"/>
<control-output control="FLAP1" prop="/surface-positions/aileron-pos-norm"/>
<control-output control="SLAT" prop="/surface-positions/flap-pos-norm"/>
<control-speed control="SLAT" transition-time="1.1"/>
<control-speed control="FLAP0" transition-time="15"/>
<control-speed control="FLAP1" transition-time="1.2"/>
</wing>
<mstab x="3.0" y="0.372" z="0.3"
chord="5.1"
length="4.9"
taper="0.9"
incidence="1.7"
sweep="80"
dihedral="0"
camber="-0.05">
<stall aoa="18" width="2" peak="1.3"/>
</mstab>
<mstab x="-2.0" y="0" z="0.3"
chord="4.1"
length="1.283"
taper="1.0"
incidence="1.7"
sweep="0"
dihedral="0"
camber="-0.05">
<stall aoa="18" width="2" peak="1.3"/>
<flap0 start="0.01" end="0.47" lift="0" drag="35.9"/>
<control-input axis="/controls/flight/speedbrake" control="FLAP0"/>
<control-output control="FLAP0" prop="/surface-positions/speedbrake-pos-norm"/>
<control-speed control="FLAP0" transition-time="4"/>
</mstab>
<hstab x="-6.15" y="1.1" z="0.2"
taper="0.423"
length="2.8"
chord="2.652"
sweep="32"
dihedral="0">
<stall aoa="30" width="13" peak="1.5"/>
<flap0 start="0" end="1.4" lift="3.3" drag="1.2"/>
<flap1 start="0.0" end="0.75" lift="1.0" drag="6.8"/>
<control-input axis="/controls/flight/elevator" control="FLAP0"/>
<control-input axis="/controls/flight/elevator-trim" control="FLAP0"/>
<control-input axis="/controls/flight/speedbrake" control="FLAP1"/>
<control-output control="FLAP0" prop="/surface-positions/elevator-pos-norm"/>
<control-output control="FLAP1" prop="/surface-positions/speedbrake-pos-norm"/>
<control-speed control="FLAP0" transition-time="0.8"/>
<control-speed control="FLAP1" transition-time="3.0"/>
</hstab>
<vstab x="-4.615" y="1.0" z="0.5"
taper="0.447"
length="2.7"
chord="2.8"
sweep="27"
dihedral="70.0">
<stall aoa="27" width="10" peak="1.5"/>
<flap0 start="0" end=".8" lift="1.3" drag="1.3"/>
<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"/>
<control-speed control="FLAP0" transition-time="1"/>
</vstab>
<vstab x="-4.615" y="-1.0" z="0.5"
taper="0.447"
length="2.7"
chord="2.8"
sweep="27"
dihedral="110.0">
<stall aoa="27" width="10" peak="1.5"/>
<flap0 start="0" end=".8" lift="1.3" drag="1.3"/>
<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"/>
<control-speed control="FLAP0" transition-time="1"/>
</vstab>
<jet x="-6.8" y="0.44" z="-0.18"
mass="2282"
thrust="11000"
afterburner="17750"
epr="32.1"
egt="1050"
n1-idle="25"
n1-max="105"
n2-idle="30"
n2-max="230"
exhaust-speed="1500"
rotation="0">
<actionpt x="-7.745" y="0.44" z="-0.18"/>
<control-input axis="/controls/engines/engine[0]/throttle" control="THROTTLE"/>
<control-input axis="/controls/engines/engine[0]/throttle" src0="0.85" dst0="0.0" src1="1.0" dst1="1.0" control="REHEAT"/>
<control-output control="REHEAT" prop="engines/engine[0]/afterburner" />
</jet>
<jet x="-6.8" y="-0.44" z="-0.18"
mass="2282"
thrust="11000"
afterburner="17750"
epr="32.1"
egt="1050"
n1-idle="25"
n1-max="105"
n2-idle="30"
n2-max="230"
exhaust-speed="1500"
rotation="0">
<actionpt x="-7.745" y="-0.44" z="-0.18"/>
<control-input axis="/controls/engines/engine[1]/throttle" control="THROTTLE"/>
<control-input axis="/controls/engines/engine[1]/throttle" src0="0.85" dst0="0.0" src1="1.0" dst1="1.0" control="REHEAT"/>
<control-output control="REHEAT" prop="engines/engine[1]/afterburner" />
</jet>
<!-- gear -->
<!-- nose -->
<gear x="3.0" y="0" z="-1.939"
retract-time="8"
compression="0.7"
spring="1.1"
damp="1.4">
<control-input axis="/controls/flight/rudder" control="STEER" square="false"/>
<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="7"/>
</gear>
<!-- left main -->
<gear x="-2.1" y="1.570" z="-1.935"
retract-time="8"
compression="0.8"
spring="0.85"
damp="2">
<control-input axis="/controls/gear/brake-left" 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="8"/>
<control-speed control="BRAKE" transition-time="1"/>
</gear>
<!-- right main -->
<gear x="-2.1" y="-1.570" z="-1.935"
retract-time="8"
compression="0.8"
spring="0.85"
damp="2">
<control-input axis="/controls/gear/brake-right" 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="8"/>
<control-speed control="BRAKE" transition-time="1"/>
</gear>
<!-- Internal tanks -->
<tank x="1.5" y="0.0" z="0.4" jet="true" capacity="3529"/>
<tank x="-1" y="0.0" z="0.4" jet="true" capacity="3400"/>
<tank x="-1.9" y="2.5" z="0.3" jet="true" capacity="2040"/>
<tank x="-1.9" y="-2.5" z="0.3" jet="true" capacity="2040"/>
<!-- drop Tanks -->
<tank x="-1.5" y="2.33" z="-0.4" jet="true" capacity="2244"/>
<tank x="0.3" y="0.0" z="-0.9" jet="true" capacity="2244"/>
<tank x="-1.5" y="-2.33" z="-0.4" jet="true" capacity="2244"/>
<!-- ballast -->
<ballast x="5.05" y="0" z="-0.1" mass="2460"/>
<ballast x="5.74" y="0" z="-0.35" mass="1000"/>
<ballast x="4" y="0" z="0.2" mass="2000"/>
<!-- external loads -->
<!-- left -->
<weight x="-2.5" y="6" z="0.1" size="0.25" mass-prop="sim/weight[0]/weight-lb" />
<weight x="-1.5" y="3.68" z="-0.55" size="0.5" mass-prop="sim/weight[1]/weight-lb"/>
<weight x="-1.5" y="2.33" z="-0.4" size="0.7" mass-prop="sim/weight[2]/weight-lb"/>
<weight x="-1.5" y="2.6" z="-0.2" size="0.3" mass-prop="sim/weight[3]/weight-lb"/>
<weight x="-1.5" y="2.1" z="-0.2" size="0.3" mass-prop="sim/weight[4]/weight-lb"/>
<weight x="-2.5" y="1.15" z="-0.7" size="0.4" mass-prop="sim/weight[5]/weight-lb"/>
<!-- Centre -->
<weight x="0.3" y="0" z="-0.9" size="0.7" mass-prop="sim/weight[6]/weight-lb" />
<!--right -->
<weight x="-2.5" y="-1.15" z="-0.7" size="0.4" mass-prop="sim/weight[7]/weight-lb"/>
<weight x="-1.5" y="-2.1" z="-0.2" size="0.3" mass-prop="sim/weight[8]/weight-lb"/>
<weight x="-1.5" y="-2.6" z="-0.2" size="0.3" mass-prop="sim/weight[9]/weight-lb"/>
<weight x="-1.5" y="-2.33" z="-0.4" size="0.7" mass-prop="sim/weight[10]/weight-lb"/>
<weight x="-1.5" y="-3.68" z="-0.55" size="0.5" mass-prop="sim/weight[11]/weight-lb"/>
<weight x="-2.5" y="-6" z="0.1" size="0.25" mass-prop="sim/weight[12]/weight-lb"/>
<!-- Hook -->
<hook x="-6.3"
y="0.0"
z="-0.561891"
length="2.7"
down-angle="77"
up-angle="-13">
<control-input axis="/controls/gear/tailhook"
control="HEXTEND"/>
<control-speed control="HEXTEND"
transition-time="5"/>
</hook>
<!-- Launch-bar -0.780453-->
<launchbar x="3.5"
y="0.0"
z="-1.0"
length="3.5052"
down-angle="90"
up-angle="0"
holdback-x="-16.3"
holdback-y="0.0"
holdback-z="0.1175"
holdback-length="2.0">
<control-input axis="/controls/gear/launchbar"
control="LEXTEND"/>
<control-speed control="LEXTEND"
transition-time="1"/>
<control-input axis="/controls/gear/launchbar/acceleration-norm"
control="LACCEL"/>
</launchbar>
</airplane>