How Do Impulse and Work Relate in Rocket Dynamics Homework Problems?

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SUMMARY

The discussion focuses on the relationship between impulse and work in the context of rocket dynamics, specifically in hypothetical scenarios involving a rocket with a power output of 3000 watts and a gravitational force of 10 m/s². It concludes that in a hovering state, the work done is zero due to the absence of velocity, leading to zero efficiency. The need for additional information, such as mass flow rate and exit velocity, is emphasized to solve the problems presented. The distinction between impulse and work is clarified, indicating they should not be considered synonymous in this context.

PREREQUISITES
  • Understanding of basic physics concepts such as impulse and work
  • Knowledge of rocket dynamics and thrust generation
  • Familiarity with power calculations in mechanical systems
  • Basic grasp of gravitational forces and their effects on motion
NEXT STEPS
  • Research the principles of thrust and its calculation in rocket propulsion
  • Learn about the concept of mass flow rate in rocket engines
  • Study the relationship between power, work, and efficiency in mechanical systems
  • Explore the implications of gravitational forces on static and dynamic equilibrium in rockets
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Students studying physics, aerospace engineers, and anyone interested in understanding the dynamics of rocket propulsion and the principles of work and impulse in mechanical systems.

Persson
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Homework Statement


I have a hipotetic rocket that have a power of 3000 watt, however its position don't change because the effect of a gravity of 10m/s^2 do the rocket remains like it would be resting. I need to determine the mass of the rocket. In a similar problem I have a rocket also in an unchangeable altitude by the effect of the gravity with a mass of 400kg and I need to determine the power of the rocket engine.
I would like to know if I could consider in this case impulse and work as synonymous or if there's another way to solve the problem. Since there's a spend of energy by the rockets .

Homework Equations



It's not used the rocket equation, it is just a hypothetical situation to calculate the energy spend to remain a static position

The Attempt at a Solution

 
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Persson said:

Homework Statement


I have a hipotetic rocket that have a power of 3000 watt, however its position don't change because the effect of a gravity of 10m/s^2 do the rocket remains like it would be resting. I need to determine the mass of the rocket.

In a similar problem I have a rocket also in an unchangeable altitude by the effect of the gravity with a mass of 400kg and I need to determine the power of the rocket engine.
I would like to know if I could consider in this case impulse and work as synonymous or if there's another way to solve the problem. Since there's a spend of energy by the rockets .

You cannot solve either. You need more information. Do you know the mass flow rate from the rocket engine? The exit velocity?

The work done on a rocket is the thrust * velocity. When the rocket is hovering the velocity is zero. So the work done on the rocket is zero. This means the efficiency is zero. All of the work done by the rocket (or helicopter rotor) is wasted. The power required to hover depends on the efficincy of the engine.
 
Thank you so much
 

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