What is the speed of the second stage after separation?

In summary, the rocket has a total of 3m momentum after the separation of the first and second stage. The second stage has a speed of 3640.8m/s.
  • #1
MightyMan11
13
0

Homework Statement


A two-stage rocket is traveling at 1192.0 m/s with respect to the Earth when the first stage runs out of fuel. Explosive bolts release the first stage and push it backward with a speed of 32.4 m/s relative to the second stage. The first stage is 2.00 times as massive as the second stage. What is the speed of the second stage after the separation?

Homework Equations


Conversation of momentum.

The Attempt at a Solution


I first set the second stage's mass as "m". The mass of the first stage then would be "2m" and the total rocket would have a mass of "3m".
Using the conservation of momentum I made an equation:
momentum of first stage+momentum of second stage= momentum of the rocket
(-32.4)*(2m) + v(m) = 1192(3m)

the m's cancel out and I solved for v:
3,640.8 m/s

however this does not match the answer in my textbook... :/

Thanks in advanced.
 
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  • #2
push it backward with a speed of 32.4 m/s relative to the second stage.
Note the word "relative". It is highly significant!
 
  • #3
Wow,
I didn't catch that...
Does that mean then the first stage of the rocket is still moving up, just at a slower speed than the second stage? (1192-32.4=speed of first stage)?
And since the first stage is "slowing down", if momentum is conserved the second stage should "speed up"?
 
  • #4
It means that, if v1 is the fist stage's velocity, v2 the secondstage,
then we have the equation:
[tex]v_{1}-v_{2}=-34m/s\to{v}_{1}=v_{2}-34m/s[/tex]
Thus, energy conservation becomes:
[tex](2m)(v_{2}-34)+mv_{2}=(3m)1192[/tex]
Solving for v2, we get:
[tex]3mv_{2}=m(3*1192+2*34)[/tex],
which you can manage on your own.
And yes, the other stage will still be moving upwards, at approximately 1181m/s
 
  • #5
Ah.
Thank you very much for your help.
 

1. How does a rocket work?

A rocket works on the principle of Newton's Third Law of Motion, which states that for every action, there is an equal and opposite reaction. In simple terms, this means that the force of the rocket's exhaust pushing downwards creates an equal and opposite force upwards, propelling the rocket upwards.

2. What is the difference between a rocket and a jet?

A jet engine works by taking in air, compressing it, and then mixing it with fuel before igniting it. This creates a continuous thrust that propels the jet forward. In contrast, a rocket carries its own supply of fuel and oxidizer and does not require air to create thrust. It is also not limited by the speed of air like a jet engine, making it more suitable for space travel.

3. How fast can a rocket travel?

The speed of a rocket depends on various factors such as the amount of fuel it carries, the design of the rocket, and the amount of drag it encounters. However, the fastest speed achieved by a rocket was during NASA's New Horizons mission, which reached a speed of about 36,373 miles per hour or 58,536 kilometers per hour.

4. Can a rocket work in space?

Yes, a rocket can work in space. As mentioned before, a rocket does not require air to create thrust, so it can function in the vacuum of space. However, it will eventually run out of fuel and stop accelerating, which is why rockets often have multiple stages that can be discarded once their fuel is depleted.

5. How does a rocket change direction?

A rocket can change direction by altering the direction of its thrust. This can be achieved by using thrusters, which are small rockets located on the sides of the main rocket. By firing these thrusters, the rocket can change its direction and angle of flight.

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