Calculating the escape speed and gravity of a planet / moon

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Homework Help Overview

The discussion revolves around calculating the acceleration of gravity, escape speed, and orbital speed for a moon named Dactyl, which orbits the asteroid Ida. The problem involves applying gravitational formulas to determine these values based on the moon's mass and radius.

Discussion Character

  • Exploratory, Assumption checking

Approaches and Questions Raised

  • The original poster attempts to calculate the acceleration of gravity, escape speed, and orbital speed using provided formulas. Some participants question the reporting of significant figures in the results, suggesting that the original poster should consider the significant figures used in the problem statement.

Discussion Status

The discussion includes verification of the calculations presented by the original poster, with some participants offering feedback on the importance of significant figures. There is an ongoing exploration of how to appropriately report results based on the information given in the problem.

Contextual Notes

Participants note that the teacher did not specify the number of significant figures to use, leading to a discussion about how to determine this based on the problem's context.

mr_miyagi
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Problem:
One of the asteroids, Ida, looks like an elongated potato. Surprisingly it has a tiny (compared to Ida) spherical moon! This moon called Dactyl has a mass of 4.20x1016kg, and a radius of 1.57x104 meters, according to Wikipedia.
Solve:
- Find the acceleration of gravity on the surface of Dactyl.
- Find the escape speed on Dactyl.
- If you are 10,000 meters above the surface of Dactyl, what must your orbital speed be?

I want to make sure that I've solved the problem correctly. Can anyone check my work?

What have I done:
- Calculate the acceleration of gravity:
F = (G*M)/R2 = (6.67384*10-11 * 4.20*1016) / (1.57*104)2 = 0.0113717 m/s2 = 11.3717 * 10-3 m/s2

Escape Speed:
I saw on wikipedia that the formula for escape speed is:
ve = sqrt((2*G*M)/r)
That would give = sqrt((2*6.67384*10-11 * 4.20*1016) / 1.57*104) = 18.8963 m/s

Orbital Speed:
Formula for orbital speed:
vo = sqrt((G*M)/r)
That would give = sqrt(6.67384*10-11 * 4.20*1016) / 1.57*104 + 10000) = 10.4434 m/s
 
Last edited:
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Values look okay!

Be sure to use use an appropriate number of significant figures when you report your results.
 
[Removed: Question already answered]
 
thx for the replies. The teacher didn't specify how many significant figures...
 
The teacher doesn't have to say how many significant figures to use. It's right there in the question. How many significant figures are used in the question?
 

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