Calculate Orbital Period of Earth: GM & a for t in Years

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In summary, the conversation revolves around finding the orbital period of Earth using a given formula and the correct units. The formula used is T(years)=\sqrt{a^{3}}, where a is the semi-major distance in Astronomical Units (au) and T is the orbital period in years. However, the conversation leads to the conclusion that the formula is not physically acceptable and that it should be in seconds instead. The final calculation uses the given formula with the correct units to find the orbital period of Earth in seconds. The conversation also emphasizes the importance of using the correct units and conversion between units in physics problems.
  • #1
DB
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Im having a little trouble finding the orbital period of Earth using:

[tex]t_{years}=2\pi\sqrt{\frac{a^3}{GM}}[/tex]

"M" being the mass of the central body, obviously the sun, at 2 x 10^30 kg
"a" being the semi-major distance in Au = 1
So,
[tex]\approx[/tex]

[tex]t_{years}=6.28\sqrt{\frac{1}{6.673*2}}*\sqrt{\frac{1}{10^{-11}*10^{30}}[/tex]

[tex]t_{years}=6.28\sqrt{.0749}*\sqrt{10^{-19}}[/tex]

[tex]t_{years}=6.28*.2736*(3.16*10^{-10})[/tex]

[tex]t_{years}=5.428*10^{-10}[/tex]

[tex]5.428*10^{-10}\neq1year[/tex]

I know I'm doing something terribly wrong, any help appreciated :biggrin:

One other question, the gravitational constant is in Newton/seconds right?
 
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  • #2
1-st question:how did u get the orbit period in HOURS?
2-nd question:are u familiar working with big numbers?

Daniel.

PS.Use the constant correctly.Together with their units.
 
  • #3
dextercioby said:
1-st question:how did u get the orbit period in HOURS?

Ya big oopps, I realize my sheet says years, I don't know why I remembered hours, ill edit that thank you.
dextercioby said:
2-nd question:are u familiar working with big numbers?
Familiar enough.
 
  • #4
WHAT?It should be in SECONDS,because every other constant (in the RHS) is in SI units...

Daniel.

PS.Post your work.Again,pay attention with your units.
The result should be roughly [tex] \pi\cdot 10^{7} s [/tex].
 
  • #5
You need to get all of quantities in the same units. Make it a habit to write the physical units of all of your quantities. What are your units of length? Are they the same in both the numerator and denominator?
 
  • #6
When working with problems like these, you should be sure to convert to SI units. ie 1 Year = 3600 x 24 x 365 seconds.
If you are methodical in doing this everytime, you should avoid further problems.

And if required in the end result, you can convert back to years again without messing with your working.

Also AU is NOT the unit you want to be using for length. Convert to metres.

I think you need to take some classes on dimensional analysis...has anyone got any good links for that?
 
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  • #7
Thanks. I am confused though. I've been wroking it out over and over and keep getting weird answers, I really can't see what to change. Should "a" be in metres because G is in m^3 kg^-1/s^2 ?

And take a look here:
http://en.wikipedia.org/wiki/Orbital_period
under Small body orbiting a central body it says t is in years and a is au's.
 
  • #8
O i just saw your reply kirovman, thanks I am going to keep trying.
 
  • #9
DB said:
Thanks. I am confused though. I've been wroking it out over and over and keep getting weird answers, I really can't see what to change. Should "a" be in metres because G is in m^3 kg^-1/s^2 ?

And take a look here:
http://en.wikipedia.org/wiki/Orbital_period
under Small body orbiting a central body it says t is in years and a is au's.


I believe the problem is asking for the orbital period in seconds.We all know that the orbital period of Earth is 1 year,but we want to find that using physics and not our senses.

That formula
[tex] T(years)=\sqrt{a^{3}} [/tex] is not physically acceptable/correct.

Daniel.

PS.Physics is rigor.Dimensional analysis of mathematical expressions is essential.
 
  • #10
Bingo. Thanks guys. I'm happy :smile:

[tex]t_s=2\pi\sqrt{\frac{(149597887000 m)^3}{6.67 m^3/kg/s^2 * 2 kg}}*\sqrt{\frac{1}{10^{-11}*10^{30}}[/tex]

[tex]t_s=2\pi\sqrt{\frac{3.34*10^{33} m}{13.34}}*3.16*10^{-10}[/tex]

[tex]t_s=6.28*1.58*10^{16}*3.16*10^{-10}[/tex]

[tex]t_s=\frac{\frac{31354784}{3600}}{24}=362[/tex]

I made some stupid mistakes because I find it difficult dealing with m^3/kg/s^2, but now that I found out "a" should be in metres in worked out.
I'm really just doing this for the fun of it, for the sake of learning.

Thanks all.
 
  • #11
dextercioby said:
That formula
[tex] T(years)=\sqrt{a^{3}} [/tex] is not physically acceptable/correct.

ya it caused me a lot of stress
 
  • #12
DB said:
ya it caused me a lot of stress

Advice for future physics problems involving numerical calculations:
Always use the sign/s of approximation:
[tex] \approx [/tex] or [tex] \sim [/tex]
,when dealing with nonexact figures.

In your case,all "equal to" signs should have been "appox.equal to".

Daniel.

PS.Speed of light in vacuo is the only exception.
 
  • #13
T(years) = (a^3)^(1/2) IS physically acceptable IF using units of years and Astronomical Units (units that are actually used in astrophysics quite often). Things to note are: what are your dimensions? For almost any homework problem in physics, turn the dimensions given into S.I. if not given so. However, in much astronomical research, one must take care to convert to the units given in the field. For instance, in the area of close binary systems, masses are often given and calculated in terms of the Sun's mass, lengths in terms of the Sun's radius, time in days, and you will find in the literature as much. The bottom line is know what units are applicable, and know how to convert between the two. Happy physics everyone :)
 

Related to Calculate Orbital Period of Earth: GM & a for t in Years

1. How do I calculate the orbital period of Earth?

To calculate the orbital period of Earth, you need to know two factors: the gravitational constant (GM) and the semi-major axis (a) of Earth's orbit around the sun. The equation to calculate the orbital period is T = 2π√(a^3/GM), where T is the orbital period in seconds.

2. What is the value of GM for Earth?

The value of GM for Earth is approximately 3.986 x 10^14 m^3/s^2. This value is a constant that represents the strength of the gravitational force between Earth and the sun. It is used in the equation to calculate the orbital period of Earth.

3. How do I find the semi-major axis of Earth's orbit?

The semi-major axis of Earth's orbit can be found by measuring the average distance between Earth and the sun. This distance is approximately 149.6 million kilometers or 93 million miles. Alternatively, you can also use the equation a = (r1 + r2)/2, where r1 is the closest distance between Earth and the sun (perihelion) and r2 is the farthest distance (aphelion).

4. Why is the orbital period of Earth important?

The orbital period of Earth is important because it determines the length of our calendar year. It also plays a crucial role in the Earth's seasons and climate, as the changing distance from the sun affects the amount of solar energy received by the planet.

5. Can the orbital period of Earth change?

Yes, the orbital period of Earth can change due to various factors such as gravitational interactions with other planets, changes in the Earth's orbit, and changes in the mass of the sun. However, these changes are very small and occur over long periods of time.

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