Consider a jet aircraft executing a level turn at a constant altitude. The aircraft has the

following characteristics:

Weight of the aircraft, $W=50000N$

Speed during the turn, $V_s=120\frac{m}{s}$

The bank angle is $45$ degrees.

Compute the total lift required for the aircraft to maintain a steady level turn at a bank angle

of $45.(4$pts$)$

Calculate the radius of the turn. $(4$pts$)$

Compute the load factor experienced by the aircraft during this maneuver. $(4$ pts $)$

Determine the rate of turn $($in degrees per second$).(4$ pts $)$