What is the acceleration of the rocket?

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SUMMARY

The discussion focuses on calculating the acceleration of a rocket emitting gas at a speed of 1500 m/sec with a flow rate of 100 kg/sec and a net mass of 5000 kg. Using the conservation of momentum, the upward velocity of the rocket was determined to be 30 m/s. The participants emphasized the importance of applying Newton's second law and correctly accounting for changing mass and velocity in the momentum equations. The key takeaway is that the acceleration can be derived from the change in momentum over time, considering the rocket's mass loss due to gas emission.

PREREQUISITES
  • Understanding of Newton's second law (F=ma)
  • Familiarity with conservation of momentum principles
  • Knowledge of calculus, specifically differentiation (d(mv)/dt)
  • Basic concepts of rocket propulsion and mass flow rates
NEXT STEPS
  • Study the derivation of Newton's second law from momentum principles
  • Learn about variable mass systems in classical mechanics
  • Explore advanced topics in rocket propulsion, including thrust equations
  • Investigate the application of calculus in physics problems involving changing quantities
USEFUL FOR

Physics students, aerospace engineers, and anyone interested in understanding rocket dynamics and the principles of motion involving variable mass systems.

kalupahana
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1. Problem
A launched rocket emitting gas with a speed of 1500 m/sec relative to rocket and with flowrate of 100 kg/sec.
If net mass of rocket is 5000 kg, find it's acceleration.

2. Equations
F=ma
F=d(mv)/dt
Conservation of momentum
m1u1 + m2u2 = m1v1 + m2v2

3.Attempt
Flowrate = 100 kg/s
velocity = 1500 m/s
momentum downwards = mv = 100 x 1500 = 1.5 x 105 kg m/s

According to conservation of momentum, i found the velocity to upward direction.

m1u1 + m2u2 = m1v1 + m2v2
0 = -100 x 1500 + 5000v2
5v2 = 150
v2 = 30 m/s

what should do next to find the acceleration
If I use F=d(mv)/dt
what is the initial velocity and final velocity. I have no idea about those two & and how to take it.
 
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Hello!
usually those kind of problems are done first writing momentum at the time t, then at the time t+dt, taking difference P(t+dt)-P(t) and dividing it by dt, then you will get Newton's second law: F= dP/dt, with no external forces F = 0. If you'll get correct expression for P(t) and P(t+dt), then acceleration will pop up in dP/dt expression. just don't forget that mass is changing, and so is velocity, and that gas emitting speed is given relative to the rocket - in writing momentum you need its speed relative to inertial frame (one that is not accelerating).
 

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