<airplane mass="400000"> <!-- Approach configuration --> <approach speed="130" aoa="9"> <control axis="/controls/throttle[0]" value="0.5"/> <control axis="/controls/throttle[1]" value="0.5"/> <control axis="/controls/flaps" value="1.0"/> </approach> <!-- Cruise configuration --> <cruise speed="487" alt="41000"> <control axis="/controls/throttle[0]" value="1.0"/> <control axis="/controls/throttle[1]" value="1.0"/> <control axis="/controls/flaps" value="0.0"/> </cruise> <cockpit x="-5.42" y="1.81" z="15.06"/> <fuselage ax="0" ay="0" az="0" bx="-69.86" by="0.00" bz="2.41" width="6"/> <wing x="-26.50" y="3.01" z="-1.45" length="33.72" chord="13.25" sweep="33" taper=".27" dihedral="7" camber="0.1"> <stall aoa="15" width="2" peak="1.5"/> <flap0 start="0" end=".56" lift="1.8" drag="3"/> <flap1 start=".64" end=".88" lift="1.3" drag="1.5"/> <control axis="/controls/flaps" output="FLAP0"/> <control axis="/controls/aileron" output="FLAP1" split="true"/> </wing> <hstab x="-62.63" y="1.81" z="1.81" chord="8.43" length="10.84" taper=".29" sweep="28" dihedral="7" effectiveness="1"> <stall aoa="15" width="2" peak="1.5"/> <flap0 start="0" end="1" lift="1.5" drag="2.0"/> <control axis="/controls/elevator" output="FLAP0"/> <control axis="/controls/elevator-trim" output="FLAP0"/> </hstab> <vstab x="-62.63" y="0.00" z="3.61" chord="12.04" length="12.04" taper="0.3" sweep="33" effectiveness="1"> <stall aoa="15" width="2" peak="1.5"/> <flap0 start="0" end="1" lift="1.2" drag="1.3"/> <control axis="/controls/rudder" output="FLAP0" invert="true"/> </vstab> <jet x="-34.93" y="16.26" z="-1.20" mass="8000" thrust="60000"> <control axis="/controls/throttle[0]" output="THROTTLE"/> </jet> <jet x="-26.50" y="12.65" z="-2.41" mass="8000" thrust="60000"> <control axis="/controls/throttle[0]" output="THROTTLE"/> </jet> <jet x="-26.50" y="-12.65" z="-2.41" mass="8000" thrust="60000"> <control axis="/controls/throttle[1]" output="THROTTLE"/> </jet> <jet x="-34.93" y="-16.26" z="-1.20" mass="8000" thrust="60000"> <control axis="/controls/throttle[1]" output="THROTTLE"/> </jet> <gear x="-5.42" y="0.00" z="-5.42" retract-time="7" compression="2"> <!-- nose --> <control axis="/controls/rudder" output="STEER" square="true"/> </gear> <gear x="-29.15" y="5.42" z="-5.42" retract-time="7" compression="2"> <!-- fwd left main --> <control axis="/controls/brakes[0]" output="BRAKE"/> </gear> <gear x="-31.32" y="1.81" z="-5.42" retract-time="7" compression="2"> <!-- rear left main --> <control axis="/controls/brakes[0]" output="BRAKE"/> </gear> <gear x="-31.32" y="-1.81" z="-5.42" retract-time="7" compression="2"> <!-- rear right main --> <control axis="/controls/brakes[1]" output="BRAKE"/> </gear> <gear x="-29.15" y="-5.42" z="-5.42" retract-time="7" compression="2"> <!-- fwd right main --> <control axis="/controls/brakes[1]" output="BRAKE"/> </gear> <tank x="-26.50" y="0" z="-1.45" jet="true" capacity="128000"/> <tank x="-30.10" y="8" z="-1.45" jet="true" capacity="128000"/> <tank x="-30.10" y="-8" z="-1.45" jet="true" capacity="128000"/> <ballast x="-6" y="0" z="2.4" mass="40000"/> <!-- hump --> <ballast x="-12" y="0" z="2.4" mass="40000"/> <!-- hump --> <ballast x="-18" y="0" z="2.4" mass="40000"/> <!-- hump --> <ballast x="-24" y="0" z="2.4" mass="40000"/> <!-- hump --> </airplane>