Escape Speed for Solar System Probe

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SUMMARY

The minimum escape speed for a probe fired from a space station orbiting the sun at the same distance as Earth is approximately 42,100 m/s. This calculation is derived from the formula v = sqrt(2*G*M/R), where G is the universal gravitational constant (6.67 x 10-11 Nm2/kg2), M is the mass of the sun (1.99 x 1030 kg), and R is the average distance from the Earth to the sun (1.5 x 1011 m). The initial miscalculation of 616,479 m/s was corrected by using the appropriate distance for R, which is the mean distance from the sun to Earth.

PREREQUISITES
  • Understanding of gravitational physics and escape velocity concepts
  • Familiarity with the universal gravitational constant (G)
  • Knowledge of the mass of the sun (1.99 x 1030 kg)
  • Ability to perform calculations involving square roots and scientific notation
NEXT STEPS
  • Study the derivation of escape velocity formulas in astrophysics
  • Learn about the heliocentric gravitational constant and its applications
  • Explore the concept of orbital mechanics and its relevance to space probes
  • Investigate the differences between escape velocities from various celestial bodies
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Astronomy students, aerospace engineers, physicists, and anyone interested in the dynamics of space travel and gravitational forces.

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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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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.
 
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?
 
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.
 
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
 
by the way, the answer should be 4.21x104 m/s
 
That's great but if he's still struggling with this after five years, he's got bigger problems... :wink:
 

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