<!-- TSR2 yasim config. This is a hack and not an authentic representation of the aircraft. Having said that, the numbers, where I could find them, roughly match those of the original aircraft. Lee Elliott. --> <airplane mass="54750"> <!-- Approach configuration --> <approach speed="180" aoa="6.0"> <control-setting axis="/controls/throttle[0]" value="0.2"/> <control-setting axis="/controls/flaps" value="3.0"/> <control-setting axis="/controls/gear-down" value="1"/> </approach> <!-- Cruise configuration --> <!-- <cruise speed="500" alt="35000"> --> <cruise speed="800" alt="35000"> --> <control-setting axis="/controls/throttle[0]" value="1.0"/> <control-setting axis="/controls/flaps" value="0.0"/> <control-setting axis="/controls/gear-down" value="0"/> </cruise> <cockpit x="-4.5" y="0.0" z="1.0"/> <fuselage ax="0" ay="0" az="0" bx="-27.13" by="0" bz=".64" width="2.0" taper="0.5" midpoint="0.3"/> <wing x="-16.0" y="1.5" z="0" taper="0.25" length="5.0" chord="6.0" sweep="50" dihedral="-1.0" camber="0.1"> <stall aoa="3.0" width="5" peak="1.3"/> <flap0 start="0.0" end="0.5" lift="2.0" drag="2.1"/> <flap1 start="0.5" end="1.0" lift="1.15" drag="1.3"/> <control-input axis="/controls/flaps" control="FLAP0"/> <control-input axis="/controls/aileron" control="FLAP1" split="true"/> <control-input axis="/controls/aileron-trim" control="FLAP1" split="true"/> <control-output control="FLAP0" prop="/surface-positions/flap-pos-norm"/> <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"/> <control-speed control="FLAP0" transition-time="5"/> </wing> <hstab x="-23.0" y="-1.0" z="0.5" taper=".2" effectiveness="1.0" length="3.0" chord="4.0" sweep="55" dihedral="-3.0"> <stall aoa="3.0" width="10" peak="1.5"/> <flap0 start="0" end="1" lift="1.7" drag="2.0"/> <control-input axis="/controls/elevator" control="FLAP0"/> <control-input axis="/controls/elevator-trim" control="FLAP0"/> <control-output control="FLAP0" prop="/surface-positions/elevator-pos-norm"/> </hstab> <vstab x="-23.0" y="0" z="1.38" taper=".176" length="4.5" chord="4.0" sweep="50"> <stall aoa="3.0" width="10" peak="1.5"/> <flap0 start="0" end="1" lift="1.15" drag="1.3"/> <control-input axis="/controls/rudder" control="FLAP0" invert="true"/> <control-output control="FLAP0" prop="/surface-positions/rudder-pos-norm"/> </vstab> <jet x="-21.0" y="-1.0" z=".44" mass="4000" thrust="16600" afterburner="30600"> <!-- <jet x="-22.0" y="-1.0" z=".44" mass="4000" thrust="30600"> --> <control-input axis="/controls/throttle[0]" control="THROTTLE"/> <control-input axis="/controls/afterburner[0]" control="REHEAT"/> </jet> <jet x="-21.0" y="1.0" z=".44" mass="4000" thrust="16600" afterburner="30600"> <!-- <jet x="-22.0" y="1.0" z=".44" mass="4000" thrust="30600"> --> <control-input axis="/controls/throttle[1]" control="THROTTLE"/> <control-input axis="/controls/afterburner[1]" control="REHEAT"/> </jet> <!-- nose --> <gear x="-8.0" y="0" z="-1.93" retract-time="7" compression="1.3"> <control-input axis="/controls/rudder" control="STEER" square="true"/> <control-input axis="/controls/gear-down" control="EXTEND"/> <control-speed control="EXTEND" transition-time="7"/> <control-output control="EXTEND" prop="/gear/gear/position-norm"/> </gear> <!-- left main --> <gear x="-19.0" y="1.19" z="-1.56" retract-time="7" compression="0.2"> <control-input axis="/controls/brakes[0]" control="BRAKE"/> <control-input axis="/controls/gear-down" control="EXTEND"/> <control-speed control="EXTEND" transition-time="7"/> <control-output control="EXTEND" prop="/gear/gear[0]/position-norm"/> </gear> <!-- right main --> <gear x="-19.0" y="-1.19" z="-1.56" retract-time="7" compression="0.2"> <control-input axis="/controls/brakes[1]" control="BRAKE"/> <control-input axis="/controls/gear-down" control="EXTEND"/> <control-speed control="EXTEND" transition-time="7"/> <control-output control="EXTEND" prop="/gear/gear[1]/position-norm"/> </gear> <tank x="-12.0" y="0" z="0.5" jet="true" capacity="11000"/> <tank x="-13.0" y="0" z="0" jet="true" capacity="12000"/> <tank x="-14.0" y="0" z="0" jet="true" capacity="12000"/> <ballast x="-11.0" y="0" z="1" mass="1000"/> <!-- avionics --> </airplane>