Answer:
The thrust of the jet engine is 4188.81 N.
Explanation:
Given that,
Speed = 260 m/s
Rate in air= 53.3 kg/s
Rate of fuel = 3.63 kg/s
Relative speed = 317 m/s
We need to calculate the rate of mass change in the rocket
Using formula of rate of mass
[tex]\dfrac{dM}{dt}=\dfrac{dM_{a}}{dt}+\dfrac{dM_{f}}{dt}[/tex]
Put the value into the formula
[tex]\dfrac{dM}{dt}=53.3+3.63[/tex]
[tex]\dfrac{dM}{dt}=56.93\ kg/s[/tex]
We need to calculate the thrust of the jet engine
Using formula of thrust
[tex]T=\dfrac{dM}{dt}u-\dfrac{dM_{a}}{dt}v[/tex]
Put the value into the formula
[tex]T=56.93\times317-53.3\times260[/tex]
[tex]T=4188.81\ N[/tex]
Hence, The thrust of the jet engine is 4188.81 N.