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F-35B-yasim.xml
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F-35B-yasim.xml
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<!-- Lockheed Martin F-35B Lightning II
F-35B Specifications ( www.lockheedmartin.co.uk )
Length 51.2 ft /15.6 m
Height 14.3 ft /4.36 m
Wingspan 35 ft /10.7 m
Wing area 460 sq ft /42.7 sq m
Horizontal tail span 21.8 ft /6.65 m
Weight empty 32,300 lb
Internal fuel capacity 13,500 lb /6,125 kg
Weapons payload 15,000 lb /6,800 kg
Standard internal weapons load Two AIM-120C air-to-air missiles
Two 1,000-pound GBU-32 JDAM guided bombs
Maximum weight 60,000 lb class
Propulsion*
(uninstalled thrust ratings) F135-PW-600
38,000 lb Max.
26,000 lb Mil.
40,500 lb Vertical
Speed (full internal weapons load) Mach 1.6 (~1,200 mph)
Combat radius(internal fuel) >450 nm /833 km
Range (internal fuel) >900 nm / 1,667 km
Max g-rating 7.0
*Maximum Power (Max) = with afterburner; Military Power (Mil) = without afterburner; Vertical = without afterburner
-->
<airplane mass="32300">
<!-- Approach configuration -->
<approach speed="150" aoa="4" fuel="0.1">
<control-setting axis="/controls/engines/engine[0]/throttle" value="0.4"/>
<control-setting axis="/controls/flight/flaps" value="0.4"/>
<control-setting axis="/controls/gear/gear-down" value="1"/>
<control-setting axis="/controls/flight/speedbrake" value="0"/>
</approach>
<!-- Cruise configuration. -->
<cruise speed="670" alt="43000" fuel="0.2">
<control-setting axis="/controls/engines/engine[0]/throttle" value="1"/>
<control-setting axis="/controls/flight/flaps" value="0.0"/>
<control-setting axis="/controls/gear/gear-down" value="0"/>
<control-setting axis="/controls/flight/speedbrake" value="0"/>
</cruise>
<!-- pilot eyepoint -->
<cockpit x="-2.72" y="0.0" z=".80"/>
<!-- fuselage -->
<fuselage ax="7.8" ay="0" az="0.3"
bx="3.9" by="0" bz="0.3"
width="1.9" taper= "0" midpoint= "1" />
<fuselage ax="4" ay="0" az="0.3"
bx="-5.0" by="0" bz="0.3"
width="1.9" taper= "0.65" midpoint= "0.0" />
<wing x="-2.1" y="1.61" z="0.381"
taper="0.31"
incidence="2.0"
twist="0"
length="3.95"
chord="5.1"
sweep="15"
dihedral="0">
<stall aoa="21" width="8" peak="1.3"/>
<flap0 start="0.0" end="0.5" lift="0.8" drag="1.5"/>
<flap1 start="0.47" end="0.8" lift="1.8" drag="1.2"/>
<slat aoa="4" start="0.0" end="0.813" lift="1.6" drag="1.3"/>
<control-input axis="/controls/flight/flaps" src0="0" src1="1" dst0="0" dst1="1" 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="/orientation/alpha-deg" src0="0.0" dst0="0.0" src1="10" dst1="1.0" control="SLAT"/>
<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/slat-pos-norm"/>
<control-speed control="SLAT" transition-time="0.5"/>
<control-speed control="FLAP0" transition-time="5"/>
<control-speed control="FLAP1" transition-time="0.5"/>
</wing>
<mstab x="-1.2" y="0" z="0.381"
taper="1"
length="1.8"
chord="9"
sweep="0"
dihedral="0">
<stall aoa="21" width="8" peak="1.3"/>
<flap0 start="0" end="0.15" lift="1.0" drag="80"/>
<control-input axis="/controls/flight/speedbrake" control="FLAP0" src0="0" src1="1" dst0="0" dst1="1"/>
<control-output control="FLAP0" prop="/surface-positions/speedbrake-pos-norm"/>
<control-speed control="FLAP0" transition-time="1.0"/>
</mstab>
<hstab x="-6.4" y="1.536" z="0.337"
taper="0.28"
length="2.17"
chord="2.862"
sweep="12"
dihedral="0">
<stall aoa="35" width="13" peak="1.5"/>
<flap0 start="0" end="1.3" lift="1.4" drag="1.5"/>
<flap1 start="0" end="0.15" lift="1.0" drag="80"/>
<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" src0="0" src1="1" dst0="0" dst1="1"/>
<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="0.9"/>
<control-speed control="FLAP1" transition-time="1.0"/>
</hstab>
<vstab x="-4.5" y="1.292" z="0.137"
taper="0.571"
length="3.2"
chord="2.443"
dihedral="70"
sweep="27" >
<stall aoa="27" width="10" peak="1.5"/>
<flap0 start="0" end=".8" lift="1.3" drag="1.3"/>
<flap1 start="0" end=".8" lift="1" drag="25"/>
<control-input axis="/controls/flight/rudder" control="FLAP0" invert="true"/>
<control-input axis="/controls/flight/rudder-trim" control="FLAP0" invert="true"/>
<control-input axis="/controls/engines/engine[0]/mixture" control="FLAP1" src0="0" src1="1" dst0="1" dst1="0"/>
<control-output control="FLAP0" prop="/surface-positions/rudder-pos-norm"/>
<control-speed control="FLAP0" transition-time="0.5"/>
<control-speed control="FLAP1" transition-time="1"/>
</vstab>
<vstab x="-4.5" y="-1.292" z="0.137"
taper="0.571"
length="3.2"
chord="2.443"
dihedral="110"
sweep="27" >
<stall aoa="27" width="10" peak="1.5"/>
<flap0 start="0" end=".8" lift="1.3" drag="1.3"/>
<flap1 start="0" end=".8" lift="1" drag="25"/>
<control-input axis="/controls/flight/rudder" control="FLAP0" invert="true"/>
<control-input axis="/controls/flight/rudder-trim" control="FLAP0" invert="true"/>
<control-input axis="/controls/engines/engine[0]/mixture" control="FLAP1" src0="0" src1="1" dst0="1" dst1="0"/>
<control-output control="FLAP0" prop="/surface-positions/rudder-pos-norm"/>
<control-speed control="FLAP0" transition-time="0.5"/>
<control-speed control="FLAP1" transition-time="1"/>
</vstab>
<jet x="-2.2" y="0.0" z="0.134"
mass="2150"
thrust="26000"
afterburner="38000"
n1-idle="55" n1-max="100" n2-idle="55" n2-max="105"
exhaust-speed="4550"
tsfc="0.7"
rotate="-95">
<actionpt x="-5.06" y="0.0" z="0.134"/>
<control-input axis="/controls/engines/engine[0]/throttle" src0="0.0" src1="0.95" dst0="0.0" dst1="1.0" control="THROTTLE"/>
<control-input axis="/controls/engines/engine[0]/reheat" src0="0.0" src1="0.95" dst0="0.0" dst1="1.0" control="REHEAT"/>
<control-speed control="THROTTLE" transition-time="1.0"/>
<control-speed control="REHEAT" transition-time="2.0" />
<control-input axis="/controls/engines/engine[0]/mixture" control="VECTOR" src0="0" src1="0.5" dst0="1" dst1="0"/>
<control-output control="REHEAT" prop="engines/engine[0]/afterburner" />
</jet>
<!-- LEFT/RIGHT FANS -->
<thruster x="-2.25" y="5.0" z="0" vx="0" vy="0" vz="1" thrust="1950">
<control-input axis="/controls/flight/aileron" control="THROTTLE"
src0="-1" src1="0" dst0="0" dst1="1"/>
</thruster>
<thruster x="-2.25" y="-5.0" z="0" vx="0" vy="0" vz="1" thrust="1950">
<control-input axis="/controls/flight/aileron" control="THROTTLE"
src0="0" src1="1" dst0="1" dst1="0"/>
</thruster>
<!-- LIFT FAN -->
<thruster x="3.5" y="0" z="0" vx="0" vy="0" vz="1" thrust="40000">
<control-input axis="/controls/flight/fan" control="THROTTLE"
src0="0" src1="1" dst0="0" dst1="1"/>
<control-speed control="THROTTLE" transition-time="1"/>
</thruster>
<!-- FAKE FANS FOR YAW VECTORING-->
<thruster x="-4" y="0.0" z="0" vx="0" vy="-1" vz="0" thrust="3500">
<control-input axis="/surface-positions/nozzle-yaw" control="THROTTLE"
src0="0" src1="1" dst0="0" dst1="1"/>
</thruster>
<thruster x="-4" y="-3.0" z="0" vx="0" vy="1" vz="0" thrust="3500">
<control-input axis="/surface-positions/nozzle-yaw" control="THROTTLE"
src0="-1" src1="0" dst0="1" dst1="0"/>
</thruster>
<!-- gear -->
<!-- nose -->
<gear x="4.16" y="0" z="-2.009"
retract-time="8"
compression="0.5" spring="0.5" upx="0" upy="0" upz="0.3">
<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="-2.90" y="2.037" z="-1.999"
retract-time="8"
compression="0.2"
spring="0.8"
damp="3">
<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="-2.90" y="-2.037" z="-1.999"
retract-time="8"
compression="0.2"
spring="0.8" damp="3">
<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>
<tank x="2.5" y="0" z="0.1" jet="true" capacity="3375"/>
<tank x="1" y="0.9" z="0.1" jet="true" capacity="845"/>
<tank x="1" y="-0.9" z="0.1" jet="true" capacity="845"/>
<tank x="-1" y="0.9" z="0.1" jet="true" capacity="845"/>
<tank x="-1" y="-0.9" z="0.1" jet="true" capacity="845"/>
<!-- left wing tank -->
<tank x="-1.5" y="1.3" z="0.181" jet="true" capacity="2652"/>
<!-- right wing tank -->
<tank x="-1.5" y="-1.3" z="0.181" jet="true" capacity="2652"/>
<tank x="-3" y="0.5" z="0.1" jet="true" capacity="720"/>
<tank x="-3" y="-0.5" z="0.1" jet="true" capacity="720"/>
<!-- left wing drop tank -->
<tank x="1.25" y="3.25" z="-0.5" jet="true" capacity="2516"/>
<!-- right wing drop tank -->
<tank x="1.25" y="-3.25" z="-0.5" jet="true" capacity="2516"/>
<ballast x="3.9" y="0.000" z="0.181" mass ="500"/>
<!--
<ballast x="-2.9" y="0.000" z="0.181" mass ="-1000"/>
-->
<!-- external loads -->
<weight x="-2.5"
y="4.95"
z="0.08"
size="0.3"
mass-prop="sim/weight[0]/weight-lb"/>
<weight x="-2.15"
y="4.27"
z="-0.1"
size="6"
mass-prop="sim/weight[1]/weight-lb"/>
<!-- Left drop tank -->
<weight x="-1.25"
y="3.25"
z="-0.5"
size="0.8"
mass-prop="sim/weight[2]/weight-lb"/>
<!-- Left internal bay -->
<weight x="-0.05"
y="0.5"
z="-0.57"
size="0.1"
mass-prop="sim/weight[3]/weight-lb"/>
<!-- Right internal bay -->
<weight x="-0.05"
y="-0.5"
z="-0.57"
size="0.1"
mass-prop="sim/weight[4]/weight-lb"/>
<!-- right drop tank -->
<weight x="-1.25"
y="-3.25"
z="-0.5"
size="0.8"
mass-prop="sim/weight[5]/weight-lb"/>
<weight x="-2.15"
y="-4.27"
z="-0.1"
size="6"
mass-prop="sim/weight[6]/weight-lb"/>
<weight x="-2.5"
y="-4.95"
z="0.08"
size="0.3"
mass-prop="sim/weight[7]/weight-lb"/>
</airplane>