Escape Speed for Solar System Probe

In summary, the conversation discusses the minimum speed needed for a small probe to escape the solar system from a space station orbiting the sun on the opposite side of the Earth. The escape speed formula is used to calculate the velocity, taking into account the mass and radius of the sun and the universal gravitation constant. Different values are suggested and compared, with the final answer being determined as 4.21x10^4 m/s.
  • #1
Honore
7
0
QUESTION:
A space station orbits the sun at the same distance as the Earth but on the opposite side of the sun. A small probe is fired away from the station. What minimum speed (m/s) does the probe need to escape the solar system?

MY UNDERSTANDING AND SOLUTION:
The escape speed v from a sphere of radius R and mass M is given by the energy-conservation equation as follows: (from "Schaum's 3000 Solved Problems in Physics" book, page 101)

(1/2)*m*v^2 = G*M*m / R where;

M: mass of the sun (=1.98*10^30 kg)
m: mass of the small probe
R: Radius of the sun (=6.95*10^8 m)
G: Universal Gravitation Constant [=6.67*10^(-11) Nm^2/kg^2]

From the equation typed in bold above;

v = sqrt(2*G*M / R) and using the numerical values v is found about

616479 m/s .

What do you think?

Thanks.
 
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  • #2
Six hundred kilometers per second?

Does that sound reasonable?

Always use your head to check your answers.



Without examining too closely, one thing I note is that you haven't calc'd the escape velocity from Earth orbit, you've calc'ed the escape velocity from the surface of the Sun: R = 695,000km. R should be Earth's orbit.
 
  • #3
That's why I had to ask.

Okay, let us take R as the distance between the sun and Earth since the problem says "A space station orbits the sun at the same distance as the Earth but on the opposite side of the sun", then v is found

51,393.77 m/s. What about this one?

Is this reasonable? Our professor says yes, but it is incorrect. So what?
 
  • #4
Are you sure your numbers were right? You're in the ballpark, but definitely wrong.

The heliocentric gravitational constant (GM) is 1.32712442076 x 10^11 km

One astronomical unit (average radius of the Earth's orbit) is 1.49597871 x 10^8 km

Just eyeballing it tells you your escape velocity will be a little less than the square root of 2000, which puts you in 40's of km/sec.
 
  • #5
your equation is right,

vescape = [2*G*M/R].5

your constants must be off

be sure to use:
G = 6.67x10-11
M = (mass of the sun) = 1.99x1030 kg
R = (mean disntance from the Earth to the sun) = 1.5x1011 meters

that should give you the right answer
 
  • #6
by the way, the answer should be 4.21x104 m/s
 
  • #7
That's great but if he's still struggling with this after five years, he's got bigger problems... :wink:
 

Related to Escape Speed for Solar System Probe

1. What is escape speed in space?

Escape speed in space is the minimum speed needed for an object to break free from the gravitational pull of a planet or other celestial body. It is the speed at which the object's kinetic energy is equal to the gravitational potential energy of the planet.

2. How is escape speed calculated?

Escape speed can be calculated using the formula v = √(2GM/r), where v is the escape speed, G is the gravitational constant, M is the mass of the planet, and r is the distance from the object to the center of the planet. This formula is based on Newton's law of gravitation.

3. Why is escape speed important in space travel?

Escape speed is important in space travel because it determines the amount of energy needed for a spacecraft to leave the gravitational pull of a planet and travel to other destinations in space. It is also used to calculate the trajectories of spacecrafts and to plan missions.

4. What is the difference between escape speed and orbital speed?

The main difference between escape speed and orbital speed is that escape speed is the minimum speed needed for an object to escape the gravitational pull of a planet, while orbital speed is the speed needed for an object to stay in orbit around a planet. In other words, escape speed is the speed needed to leave a planet, while orbital speed is the speed needed to stay in orbit around it.

5. Can escape speed change?

Yes, escape speed can change depending on the mass and radius of the planet. The larger the planet, the higher the escape speed required. It can also change if the distance between the object and the planet changes, as the gravitational force and potential energy will vary. Additionally, escape speed can be affected by other factors such as atmospheric drag and the presence of other celestial bodies.

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