How Does Rocket Ejection Rate Affect Its Acceleration?

In summary, the conversation discusses the velocity and acceleration of a rocket that is accelerating vertically and ejecting gas downwards. The solution provided includes the use of external forces and the momentum of the gas and rocket to determine the acceleration as a function of time. The issue being discussed is a potential mistake in the solution, specifically regarding the direction of the velocity of the gas.
  • #1
sapsapz
14
0

Homework Statement



A rocket is accelerating vertically, and it is ejecting gas downwards (which allows it to move upwards) at a rate of B. The gas is ejected at a velocity w relative to the rocket.
What is the velocity and acceleration of the rocket as a function of time?

Homework Equations


The Attempt at a Solution



My teacher arrived at a slightly different solution than mine, so I was hoping you could tell me what I am doing wrong. Maybe mixing up the directions somehow?

This is my solution:
We should look at a small section of time, from t to t+dt.
So ∫ Fexternal dt = P[t+dt]-P(t), and since the time is really short, Fexternal is basically constant, so we can take him out of the integral:

Fexternal * ∫dt = P[t+dt]-P[t]. The limits of integration are t to t+dt so:
Fexternal*(t+dt-t) = P[t+dt]-P[t].
Fexternal*dt = P[t+dt]-P[t].

Vg will signify the velocity of gas, and V will signify the velocity of the rocket. So Vg[t]=V[t]-w.

The momentum of the gas at time t is Bt*Vg[t], and at time t+dt is Bt*Vg[t]+B*dt*Vg[t+dt].
The momentum of the rocket at time t is m[t]v[t] and at time t+dt is m[t+dt]v[t+dt].

So:
Fexternal*dt = (m[t+dt]v[t+dt]+Bt*Vg[t]+B*dt*Vg[t+dt])-(Bt*Vg[t]+m[t]v[t]).
Fexternal*dt = m[t+dt]v[t+dt]+Bt*Vg[t]+B*dt*Vg[t+dt]-Bt*Vg[t]-m[t]v[t].
Fexternal*dt = m[t+dt]v[t+dt]+B*dt*Vg[t+dt]-m[t]v[t].

m[t+dt]=m[t]-Bdt, and Vg[t+dt]=V[t+dt]-w, so:

Fexternal*dt = (m[t]-Bdt)v[t+dt]+B*dt*(v[t+dt]-w)-m[t]v[t].
Dividing by dt:
Fexternal = (m[t]/dt - B)v[t+dt]+B*(v[t+dt]-w)-m[t]v[t]/dt.
Fexternal = v[t+dt]*m[t]/dt -B*v[t+dt]+B*V[t+dt]-Bw-m[t]v[t]/dt.
Fexternal = (m[t]/dt) * (v[t+dt] - v[t]) -Bw
Fexternal = (m[t]/dt) * dv[t] -Bw
Fexternal+Bw = (m[t]/dt) * dv[t]
(Fexternal+Bw)/m[t] = dv[t]/dt
(Fexternal+Bw)/m[t] = dv[t]/dt

Since the only external force acting on the rocket is mg downwards, then:
(-m[t]g+Bw)/m[t] = dv[t]/dt
-g+Bw/m[t] = dv[t]/dt

a[t]=-g+Bw/(m[0]-Bt)

The positive direction is upwards, so w is a negative. which means the acceleration will always be downwards...

What am I doing wrong?
 
Physics news on Phys.org
  • #2
sapsapz said:
Vg will signify the velocity of gas, and V will signify the velocity of the rocket. So Vg[t]=V[t]-w.

a[t]=-g+Bw/(m[0]-Bt)

The positive direction is upwards, so w is a negative. which means the acceleration will always be downwards...

What am I doing wrong?

You already took into account the direction of w when you wrote the minus sign in front of w for the velocity of the gas. So, w is a postive number.
 
Last edited:
  • #3
Of course... thank you!
 

FAQ: How Does Rocket Ejection Rate Affect Its Acceleration?

How does a rocket accelerate upwards?

A rocket accelerates upwards by burning fuel in its engines, creating hot exhaust gases that are expelled out of the back of the rocket. This creates a reaction force in the opposite direction, pushing the rocket upwards.

What is the role of thrust in a rocket's acceleration?

Thrust is the force that propels a rocket upward. It is generated by the burning of fuel in the rocket's engines and is the result of the rocket's Newton's Third Law of Motion - for every action, there is an equal and opposite reaction.

How does a rocket maintain its acceleration in space?

Once a rocket has escaped Earth's atmosphere and is in space, there is virtually no air resistance to slow it down. This allows the rocket to maintain its acceleration as long as its engines are firing and producing thrust. The rocket will continue to accelerate until it reaches its desired speed or until the engines are shut off.

What factors affect a rocket's acceleration?

The main factors that affect a rocket's acceleration are the amount of thrust generated by the engines and the mass of the rocket. The more thrust the engines produce, the greater the acceleration will be. On the other hand, the more massive the rocket is, the more force will be required to accelerate it.

How does gravity impact a rocket's acceleration?

Gravity does not directly affect a rocket's acceleration, as rockets are designed to overcome the force of gravity. However, gravity does play a role in the trajectory of a rocket, as the Earth's gravitational pull will cause the rocket to curve as it travels upwards.

Back
Top