A medium$-$sized jet has a $3\mathrm{.}8-$m$-$diameter fuselage

and a loaded mass of $85,000kg.$ The drag on an

airplane is primarily due to the cylindrical fuselage,

and aerodynamic shaping gives it a drag coefficient of

$0\mathrm{.}37$

Part A

How much thrust must the jet's engines provide to cruise at $250\frac{m}{s}$ at an altitude where the air density is $1\mathrm{.}3k\frac{g}{m^3}?$

Express your answer with the appropriate units.

View Available Hint$($s$)$

$F=110\mathrm{.}93$

X Incorrect; Try Again; $6$ attempts remaining