Calculating Orbital Speed of a Satellite Orbiting Jupiter | Step-by-Step Guide"

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Homework Help Overview

The discussion revolves around calculating the orbital speed of a satellite orbiting Jupiter, given specific parameters such as the satellite's altitude, Jupiter's mass, and radius. The original poster seeks assistance with the calculations involved in determining the orbital speed.

Discussion Character

  • Mathematical reasoning, Assumption checking

Approaches and Questions Raised

  • Participants discuss the formula for orbital speed and the correct application of the gravitational constant. There are questions about the arithmetic used in the calculations and the interpretation of the variables involved, particularly the use of the gravitational constant and the distance from the satellite to Jupiter.

Discussion Status

Some participants have provided guidance on the correct value of the gravitational constant and emphasized the importance of using the correct distance in calculations. There is a recognition of ongoing confusion regarding the arithmetic and the application of the formula, with multiple attempts being made without reaching a satisfactory answer.

Contextual Notes

Participants are grappling with the correct interpretation of the variables in the formula, particularly the distinction between gravitational constant and distance. There is an acknowledgment of potential arithmetic errors and the need for clarity on the values used in the calculations.

agadag
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Please help asap! Orbital speed

Homework Statement




A satellite is placed in orbit 5.19x105m above the surface of Jupiter. Jupiter has a mass of 1.90x1027kg and a radius of 7.14x107m. Find the orbital speed of the satellite.
Answer = m/s


Homework Equations



v = sqrt [GM/r]
= (5.19 * 10^5)(1.90*10^27)/ (7.14*10^7+5.19*10^5) = 3.703 *10^12 is wrong!
 
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Use G = 6.67 x 10^-11.
 


ahhh i still didn't get the right answer..? maybe I am just doing my arithmatic wrong. but why would gravity = 6.67?
 


G in the equation is the universal gravitational constant which has the value given by Delphi.For some reason you seem to have used the height of the orbit instead of G.
 


well i assumed since we don't know the gravity of that planet the length of the orbit would be equal to the G. However, I am still not able to get the right answer using either method...
 


I should say the length of the distance from the satellite to the planet... not the length of orbit...
 


G is the universal gravitational constant,it applies to all planets,all masses,everything,it is completely different to distance.My best advice is to look at the theory behind this otherwise you are just fiddling around. To get the right answer you just need to plug the right numbers in your calculator.In your original attempt you had the wrong value for G so try again.
 


yea i tried it again. still no success. I think i give up now.
 


agadag said:
yea i tried it again. still no success. I think i give up now.

Did you calculate the right value for r?
7.14*10^7+5.19*10^5=7.19*10^7(approximately)
Did you take the square root at the end?
 

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