What is the acceleration of the rocket?

In summary, the problem involves a rocket emitting gas at a speed of 1500 m/sec and a flowrate of 100 kg/sec, with a net mass of 5000 kg. Using the equations F=ma and F=d(mv)/dt, and applying the conservation of momentum, the upward velocity of the rocket is found to be 30 m/s. To find the acceleration, one must use the expression F=dP/dt and take into account the changing mass and velocity of the rocket, as well as the fact that the gas emitting speed is relative to the rocket's frame.
  • #1
kalupahana
36
0
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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  • #2
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).
 

FAQ: What is the acceleration of the rocket?

What is acceleration?

Acceleration is the rate at which an object's velocity changes over time. It is a measure of how quickly an object's speed is increasing or decreasing.

How is acceleration calculated?

Acceleration is calculated by dividing the change in an object's velocity by the time it takes for that change to occur. The formula for acceleration is a = (vf - vi) / t, where a is acceleration, vf is final velocity, vi is initial velocity, and t is time.

How does acceleration affect a rocket?

Acceleration is crucial for a rocket's flight. During launch, the rocket's engines provide a high amount of thrust, which causes the rocket to accelerate rapidly. This acceleration allows the rocket to overcome the force of gravity and reach outer space.

What factors can affect the acceleration of a rocket?

The acceleration of a rocket can be affected by various factors, such as the amount of thrust produced by the rocket's engines, the mass of the rocket, and external forces like air resistance. Additionally, the direction and angle of the rocket's engines can also impact its acceleration.

How is acceleration measured during a rocket launch?

Acceleration during a rocket launch is typically measured using accelerometers, which are devices that can detect and measure changes in acceleration. These devices are placed inside the rocket to gather data on the rocket's acceleration and can provide valuable information for the rocket's trajectory and performance.

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