Compression of a Spring on an Asteroid?

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Homework Help Overview

The problem involves launching a package from an airless asteroid using a compressed spring. The goal is to determine the necessary compression of the spring so that the package reaches a specific distance from the asteroid's center before being picked up by a ship.

Discussion Character

  • Exploratory, Conceptual clarification, Mathematical reasoning

Approaches and Questions Raised

  • Participants discuss the application of conservation of energy principles, comparing gravitational potential energy and spring potential energy. There are attempts to manipulate equations to derive the required spring compression.

Discussion Status

Some participants are exploring algebraic manipulations and questioning their results, while others are providing guidance on the conservation of energy approach. There is an ongoing dialogue about the correctness of the derived expressions and the assumptions made in the calculations.

Contextual Notes

Participants are navigating potential errors in algebraic manipulation and discussing the implications of the gravitational forces involved, as well as the specific distances related to the asteroid's radius.

smedearis
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Homework Statement


A package with mass m sits on an airless asteroid of mass M and radius R. We want to launch a package straight up in such a way that its speed drops to zero when it is a distance 4R away from the center of the asteroid, where it's picked up by a waiting ship before it can fall back down. We have a powerful spring whose stiffness is Ks. How much must we compress the spring?


Homework Equations


I'm not quite sure what equations to use, except I'm almost positive we're going to use U(spring)= 1/2*Ks*s^2, where s is the abs value of the stretch/compression.
Maybe also use:
F(grav)=-G((M*m)/(|r21|^2))*rhat, where |r21| is the magnitude of the difference of locations between these two objects
or:
U(grav)=-G(M*m)/|r21|


The Attempt at a Solution



I know that the answer is: stretch=sqrt((3*G*m*M)/(2*R*Ks))
I just can't figure out how to get there. I assumed that the way we got the "3" on the top was due to the actual distance between them was 3R (since 1R was the actual radius of the asteroid.

please help!
 
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You are on the right track with your equations. Consider conservation of enegy.
 
If i chose the system where everything is in the system, there is no work external. SO, Ugrav=-Uspring, b/c Delta K and Delta mc^2 go to zero.

but the answer is sqrt((3GmM)/(2Rks)) whereas my answer gives me:
sqrt((2GmM)/(3Rks)). what am i missing?
 
I think that you are simply making a manipulation error.

So we have conservation of energy;

Ugi + Uspring = Ugf

[tex]-\frac{GM}{R} + \frac{1}{2}k_{s}\cdot s^2 = -\frac{GM}{4R}[/tex]

Can you now go from here?
 
but doesn't that answer give me a 3 on the bottom and a 2 on the top? The answer has a 3 on the top and a 2 on the bottom. Am I doing my algebraic manipulation wrong?
 
Sorry, yes it does. I was reading your answers the wrong way round. From what I can see you have done nothing wrong, in my opinion your answer is correct. Perhaps, someone else can see the error?
 
smedearis said:
but doesn't that answer give me a 3 on the bottom and a 2 on the top? The answer has a 3 on the top and a 2 on the bottom. Am I doing my algebraic manipulation wrong?
You must be if you're getting the answer you got.

Consider this:
[tex]-a + x = -\frac{a}{4}[/tex]

That gives you:
[tex]x = \frac{3a}{4}[/tex]

Apply this manipulation and you'll get the expected answer.
 

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