Period of satellite in circular orbit

AI Thread Summary
The discussion revolves around calculating the orbital period of a satellite above a planet's surface using gravitational formulas. The user initially struggles with the correct application of formulas and calculations, leading to incorrect period results. After receiving guidance, they revise their calculations using the correct formula for the period, T = 2π√(R^3/GM), and adjust their values for mass and radius. The final calculations yield a period of approximately 46084.23 seconds, which is confirmed as correct when expressed with appropriate significant figures. The conversation emphasizes the importance of correctly incorporating the planet's radius and mass in orbital calculations.
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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