Period of satellite in circular orbit

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Homework Help Overview

The discussion revolves around calculating the period of a satellite in a circular orbit given specific parameters, including gravitational constant and surface gravity of a planet. The problem involves concepts from gravitational physics and orbital mechanics.

Discussion Character

  • Exploratory, Mathematical reasoning, Assumption checking

Approaches and Questions Raised

  • Participants discuss the use of various equations related to gravitational force and orbital period. There are attempts to clarify the correct application of formulas and to identify potential calculation errors.

Discussion Status

Some participants have provided guidance on the correct formulation of the period equation, while others are re-evaluating their calculations based on feedback. Multiple interpretations of the problem setup are being explored, particularly regarding the inclusion of height in mass calculations.

Contextual Notes

There is an ongoing discussion about the significance of the surface gravity value and its implications for the calculations. Participants are also addressing the importance of significant figures in their final answers.

bmoore509
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Homework Statement



Given: G = 6.67259 × 10−11 Nm2/kg2
The acceleration of gravity on the surface
of a planet of radius R = 4190 km is 6.5 m/s2.
What is the period T of a satellite in circu-
lar orbit h = 14120.3 km above the surface?
Answer in units of s.

Homework Equations


a=G(m/r^2)
T = 2πR/V
V = sqrt(GM/R)
T = 2πR/sqrt(GM/R)

The Attempt at a Solution



My formulas might be incorrect but I really don't think they are. Yet I can't seem to get the right answer.

6.5 m/s2 = (6.67259 × 10−11 Nm2/kg2) (m/((4190000m+14120300m)^2))
m=3.265952291x1025

T = 2piR/sqrt(GM/R)

= 2*pi*(4190000+14120300)/ sqrt((6.67259 × 10−11 *3.265952291x1025)/(4190000m+14120300m)

=1054559091seconds

But that answer isn't right. Any help please?
 
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The equations look correct, so I guess you made a calculation error in the last expression.

Note, that the period usually is written with the two R's combined into one, like
T = 2\pi\sqrt{\frac{R^3}{GM}}
 
bmoore509 said:
6.5 m/s2 = (6.67259 × 10−11 Nm2/kg2) (m/((4190000m+14120300m)^2))

6.5 m/s^2 is the acceleration at the surface of the planet, r=4190 km.

ehild
 
I redid my work using the formula as you wrote it.

T = 2pi (sqrt((R^3)/GM))

R3= (4190000+14120300)3 = 6.138840926x1021

G*M = (6.6725x10-11)*(3.265952291x1025)=2.17923606x1015

sqrt ( R3/(G*M) = sqrt (6.138840926x1021/2.17923606x1015) = sqrt (281696.23) = 1678.382921

T=2pi(sqrt(r^3/GM)
= 2*pi*1678.382921 = 10545.59091

Which isn't the right answer. Can you tell me where I'm going wrong?
 
Oh! Thank you! Let me rework this then.
 
T = 2pi (sqrt((R^3)/GM))

R3= (4190000+14120300)3 = 6.138840926x1021

G*M = (6.67259x10-11)*(1.710200237x1024)=1.1411465x1014

sqrt ( R3/(G*M) = sqrt (6.138840926x1021/1.1411465x1014) = sqrt (53795379.7) = 7334.533366

T=2pi(sqrt(r^3/GM)
= 2*pi*7334.533366 = 46084.23228


Does that look correct?
 
Yes, if you mean seconds. But use only 6 significant digits, and write out the units.

ehild
 
ehild said:
6.5 m/s^2 is the acceleration at the surface of the planet, r=4190 km.

Ah, I missed that the height wrongly was "included" in the calculation of planet mass. My apologies to the original poster.
 

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