Calculating Escape Velocity of Mars from the Sun's gravitational field

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Homework Help Overview

The problem involves calculating whether Mars can escape the Sun's gravitational field given its current orbital speed and distance from the Sun. The original poster attempts to determine the escape velocity of Mars based on its speed of 30000 m/s and its distance of 2.3 * 10^10 m from the Sun.

Discussion Character

  • Exploratory, Assumption checking, Conceptual clarification

Approaches and Questions Raised

  • Participants discuss the use of gravitational and orbital formulas, including the relationship between centripetal force and gravitational force. There are attempts to calculate escape velocity and questions about the relevance of Kepler's laws in this context. Some participants express uncertainty about the calculations and the implications of the escape velocity results.

Discussion Status

The discussion includes various calculations and interpretations regarding escape velocity. Some participants have provided numerical results for escape velocity, while others are questioning the accuracy of their methods and assumptions. There is a recognition that Mars's speed of 30000 m/s is insufficient for escape based on the calculations presented.

Contextual Notes

Participants note the lack of clarity regarding the edge of the solar system and the specific conditions under which Mars's escape velocity is being evaluated. There is also mention of differing interpretations of the calculations and the relevance of different physical laws.

QuickSkope
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1) The problem:
Mars orbits the Sun at a distance of 2.3 * 10^10 m with a speed of 24000 m/s. If it's speed were increased to 30000 m/s, at a time when no other planet was nearby, would Mars leave the Solar System.

2) Fc=Fg
Orbit formulas and such

3) I'm assuming you have to find the escape velocity of Mars, and use it to see if it gets out of the field. But I'm not sure, any help would be awesome :)

Edit 1) Fc=Fg
V^2=GM/r

30000^2=(6.67 * 10^-11)(1.98*10^30)/r

R= 1.467 * 10^11

I'm not sure where the edge of the solar system is, and I doubt that's right. But worth a shot.
 
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QuickSkope said:
1) The problem:
Mars orbits the Sun at a distance of 2.3 * 10^10 m with a speed of 24000 m/s. If it's speed were increased to 30000 m/s, at a time when no other planet was nearby, would Mars leave the Solar System.

2) Fc=Fg
Orbit formulas and such

3) I'm assuming you have to find the escape velocity of Mars, and use it to see if it gets out of the field. But I'm not sure, any help would be awesome :)

Edit 1) Fc=Fg
V^2=GM/r

30000^2=(6.67 * 10^-11)(1.98*10^30)/r

R= 1.467 * 10^11

I'm not sure where the edge of the solar system is, and I doubt that's right. But worth a shot.
Try using Kepler's third law .
 
I have yet to learn Keplers law, so looking it up tells me:

The*square*of the*orbital period*of a planet isproportional*to the*cube*of the*semi-major axis*of its orbit.

I'm not really sure how I'd use that, but I'll find the current period of one rotation of Mars.

Period of Mars 6.0 * 10^7

Upon further investigation, we learned the formula (4(pi^2)r/T^2) = (GM/r^2), which is a representation of Kepler third law.

Also, is the method I used not a simplification of Keplers Third Law?
 
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QuickSkope said:
I have yet to learn Keplers law, so looking it up tells me:

The*square*of the*orbital period*of a planet isproportional*to the*cube*of the*semi-major axis*of its orbit.

I'm not really sure how I'd use that, but I'll find the current period of one rotation of Mars.

Period of Mars 6.0 * 10^7

Upon further investigation, we learned the formula (4(pi^2)r/T^2) = (GM/r^2), which is a representation of Kepler third law.

Also, is the method I used not a simplification of Keplers Third Law?
You're right.

Using Kepler's 3rd Law was a silly idea. The 3000 m/s doesn't refer to a circular (or nearly circular) orbit.

The formula (4(pi^2)r/T^2) = (GM/r^2) that you mention is just from taking v2=GM/r and dividing by r . (FC = FG)

Do you know the escape speed for Mars orbit as regards escaping from the Sun's gravity, or know how to get it?
 
I can do it on a projectile that is leaving a planet, not sure how I'd do it on two planets.
 
The EP and Ek in the 2nd are 0, right?
 

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QuickSkope said:
I can do it on a projectile that is leaving a planet, not sure how I'd do it on two planets.
How about from one planet with the mass of the Sun and radius equal to Mars's orbit?
 
SammyS said:
How about from one planet with the mass of the Sun and radius equal to Mars's orbit?

Not sure I quite follow that. Are my other calculations not correct?

I did math in the above and got escape velocity of 33888 m/s.

Also, the escape velocity to hit something from the surface of Mars so that it does not come down is 2.4 km/s. If that helps at all.
 
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  • #10
QuickSkope said:
Not sure I quite follow that. Are my other calculations not correct?

I did math in the above and got escape velocity of 33888 m/s.

Also, the escape velocity to hit something from the surface of Mars so that it does not come down is 2.4 km/s. If that helps at all.
The 338888 m/s is what I was asking. (Actually, using the figures given in the problem, I got 33941 m/s.)

For an object that is at a distance of 2.3 * 1010 m from the Sun, 338888 m/s is the escape velocity for escaping the Sun. I.e. 338888 m/s is the velocity that Mars needs to escape the Sun's gravity.
 
  • #11
And so by that, if it is only traveling at 30000 m/s, it will in fact not escape the Suns gravitational field, and thus remain in the solar system?
 
  • #12
QuickSkope said:
And so by that, if it is only traveling at 30000 m/s, it will in fact not escape the Suns gravitational field, and thus remain in the solar system?
Correct.

There are other ways to show it.

They agree.
 
  • #13
Awesome, thanks for the help :D
 

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