Answer:
The thrust is

Step-by-step explanation:
From the question we are told that
The speed of the jet aircraft is
The rate at which the engine takes in air is

The rate at which the engine burns fuel is

The speed of the exhaust gases is

Generally the thrust of the engine is mathematically represented as
![F =[ \^ Q * ( u - v )] + (\r m * u)](https://img.qammunity.org/2021/formulas/physics/high-school/304k50eywiai24rkkvfdaytxjgrrtqytov.png)
=>
![F =[ 115 * ( 276 - 214 )] + (2.53 * 276)](https://img.qammunity.org/2021/formulas/physics/high-school/l1wtgf8z6vsrgl6cfwo90igq1s8aanpa3g.png)
=>
