Universal Gravitation on escape velocity

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SUMMARY

The minimum speed required for a spacecraft to escape the solar system from Earth's orbit is calculated using the formula v=sqrt(2GM/R), where G is the universal gravitational constant, M is the mass of the Sun, and R is the distance from the Earth to the Sun. A spacecraft achieving a maximum speed of 125,000 km/h must also consider its existing orbital velocity around the Sun to determine the additional velocity needed for solar escape. For the second part of the problem, rearranging the escape velocity formula to solve for R will provide the necessary distance from the Sun for the spacecraft to escape the solar system.

PREREQUISITES
  • Understanding of Universal Gravitation and escape velocity concepts
  • Familiarity with the formula v=sqrt(2GM/R)
  • Knowledge of the mass of the Sun and the universal gravitational constant (G)
  • Basic understanding of orbital mechanics and velocities
NEXT STEPS
  • Research how to rearrange gravitational formulas to solve for different variables
  • Learn about the concept of orbital velocity and its impact on escape velocity
  • Study the distances of the planets from the Sun to understand solar system dynamics
  • Explore the implications of spacecraft speeds in relation to gravitational forces
USEFUL FOR

Astronomy students, aerospace engineers, physicists, and anyone interested in understanding the mechanics of spacecraft escape velocities and solar system dynamics.

tubworld
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On dealing with Universal Gravitation topic, I came across this question:
what is the min speed, relative to the sun, necessary for a spacecraft to escape the solar system if it starts at the Earth's orbit?

My working:

v=sqrt(2GM/R), where G=universal constant, R= distance between Earth and sun and m= mass of sun. Is that all?

The second part of it states that a spaceship achieved a max speed of 125000km/h on its way to photograph jupiter. Beyond what distance from the sun is this speed sufficient to escape the solar system?

for the second part, any hints? I am getting stuck. Do i need to know the order of the planets for the second part?
 
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add on my 2 cents worth

Something just came to me: for part a do i need to consider the escape speed to leave the Earth as well. (i.e. escape speed to leave Earth + escape speed to leave sun)?
 
tubworld said:
On dealing with Universal Gravitation topic, I came across this question:
what is the min speed, relative to the sun, necessary for a spacecraft to escape the solar system if it starts at the Earth's orbit?
My working:
v=sqrt(2GM/R), where G=universal constant, R= distance between Earth and sun and m= mass of sun. Is that all?
The second part of it states that a spaceship achieved a max speed of 125000km/h on its way to photograph jupiter. Beyond what distance from the sun is this speed sufficient to escape the solar system?
for the second part, any hints? I am getting stuck. Do i need to know the order of the planets for the second part?

As for the first part, if your spacecraft is moving in Earth's orbit around the Sun it already has some orbital velocity and you need to take this into account when calculating how much additional velocity is needed to reach solar escape velocity. I would not worry about earrh escape velocity as the problem does not say that you are starting on the surface of the Earth.

For the second part, try re-arranging your formula so that it solves for R rather than V.
 

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