Work/energy/kinematics rocket ship problem

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To determine the required thrust for a rocket with an initial mass of 2.85x10^6 kg and an acceleration of 0.20g, the force must account for both the rocket's mass and gravitational pull. The thrust can be calculated using the equation F = m_rkt * (a_rkt + g), where g is the acceleration due to gravity. Additionally, with a fuel burn rate of 14,500 kg/s, the speed of the ejected gas can be found using the relationship between thrust and the rate of change of momentum. The discussion emphasizes the need to apply these principles to solve for the thrust and gas velocity effectively. Understanding these dynamics is crucial for solving rocket propulsion problems.
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Homework Statement


A rocket of initial mass of 2.85x10^6 kg is on the surface of the earth. if the initial acceleration is .20g, what is the required thrust? if the fuel is burned at a rate of 14,500 kg/s, with what speed is it ejected from the rocket?


Homework Equations





The Attempt at a Solution



The only thing i thought to do was convert the mass and acceleration of the rocket into Newtons. I also tried making the mass of the rocket into the rate of the fuel burning and tried to find how many seconds it would take to finish burning, but that was just a desperate attempt.
 
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1barcafan said:

Homework Statement


A rocket of initial mass of 2.85x10^6 kg is on the surface of the earth. if the initial acceleration is .20g, what is the required thrust? if the fuel is burned at a rate of 14,500 kg/s, with what speed is it ejected from the rocket?

Homework Equations

The force accelerating the rocket (the rate of change of momentum of the rocket + gravity) is equal and opposite to the rate of change of of momentum of the ejected rocket gases.

\vec{F} = m_{rkt}a_{rkt} + m_{rkt}g = dp_{gas}/dt = v_{gas}dm_{gas}/dt

You are given all but vgas.

AM
 
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