Work/energy/kinematics rocket ship problem

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SUMMARY

The discussion focuses on calculating the required thrust for a rocket with an initial mass of 2.85x106 kg and an initial acceleration of 0.20g. The thrust can be determined using the equation F = mrocketarocket + mrocketg, where g is the acceleration due to gravity. Additionally, the fuel is burned at a rate of 14,500 kg/s, and the speed at which it is ejected from the rocket can be calculated using the relationship between thrust and the rate of change of momentum of the ejected gases.

PREREQUISITES
  • Understanding of Newton's Second Law of Motion
  • Familiarity with the concept of thrust in rocketry
  • Knowledge of gravitational acceleration (g = 9.81 m/s2)
  • Basic principles of momentum and mass flow rate
NEXT STEPS
  • Calculate the required thrust using F = mrocketarocket + mrocketg
  • Determine the speed of the ejected gases using the thrust and mass flow rate
  • Explore the implications of varying the fuel burn rate on rocket performance
  • Investigate the effects of different gravitational environments on thrust requirements
USEFUL FOR

Students studying physics, aerospace engineers, and anyone interested in rocket propulsion and dynamics.

1barcafan
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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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