Minimum Satellite Period problem

In summary, the conversation discusses the time it takes for a watermelon to return to the hand when dropped through a tunnel in the Earth, and how this relates to the orbital period of an object around the Earth. The conversation also touches on the idea of a minimum energy subway tunnel and the transit time for different shapes. Some participants question the accuracy of the calculations due to factors such as the Earth's variable density and the effects of gravity at different points on the Earth.
  • #1
Eric M. Jones
11
0
Clever guy that I am, I am writing a small paper on Celestial Mechanics...simplified...really really simplified. However, if I bore a tunnel through the Earth and drop a watermelon through it, the watermelon returns to my hand in 76 minutes. This is an example of an elliptical orbit of e=1

But if I use the same figures and shoot the watermelon around the Earth in a grazing orbit, with eccentricity of zero, the orbital period is 6 minutes longer.

Why?

BTW: I suspect any minimum energy subway tunnel of hypocycloidal shape has 1/2 the transit time of the watermelon, or 38 minutes, or 76 minutes round trip. A hypocycloid where the generating circle diameter is the same as the base circle radius generates a straight line through the center.

Comments?
 
Physics news on Phys.org
  • #2
How did you get these figures? The formula for the period should be the same for both cases. And the value around 84 minutes.
 
  • #3
Mean Earth Radius=6.37 x10E6 meters
a=9.8 m/sec/sec (-)s=1/2at^2
solve for t: t=19.00 minutes. (time for round trip...76 minutes)
So what happened to the 8 minutes...(or the 6)?

Eric
 
  • #4
I'm only guessing here, but is it possible that the 84 minutes minimum orbit time includes the Earth's rotation? I.E. Cape Canaveral has moved eastward by 8 minutes of rotation during the orbit time? If you shot up a satellite (to the east to gain velocity), then it would be 76 minutes, +8 minutes (e.g.) before it was overhead.

?
 
  • #5
Eric M. Jones said:
Mean Earth Radius=6.37 x10E6 meters
a=9.8 m/sec/sec (-)s=1/2at^2
solve for t: t=19.00 minutes. (time for round trip...76 minutes)
So what happened to the 8 minutes...(or the 6)?

Eric

This does not make sense.
The motion through the tunnel is not uniform accelerated. The motion in the tunnel is harmonic oscillation. Write the force acting on the falling body as a function of distance from the center, to see this. Then you can use the equation from that motion.
And for the orbital motion you should use the equations for circular motion.
In the end you'll get the same formula for both periods.
Good luck.
 
  • #6
>>The motion through the tunnel is not uniform accelerated.

Isaac Newton said it was.

>>Write the force acting on the falling body as a function of distance from the center, to see this.

Okay F=ma. Gravity is considered to be simply a point in the center of the sphere.

>>And for the orbital motion you should use the equations for circular motion.

The circular motion or the elliptical motion have the same formula, and the same orbital time

Eric
 
  • #7
Eric M. Jones said:
Okay F=ma. Gravity is considered to be simply a point in the center of the sphere.

Careful - that point source rule is only valid above the surface of the earth.

When the falling object is below the surface of the Earth (requires a well or tunnel or some such) at a distance R < RE where RE is the radius of the earth, then all of the Earth that lies between R and RE forms a spherical shell with the object inside it. The gravitational field in the interior of such a shell is zero. So when you're calculating the force on the object, it's as if the mass concentrated at the point in the center of the sphere is only the mass between radius 0 and R.
 
  • #8
Thanks. The bubble of that thought came to the surface an hour ago.
 
  • #9
Eric M. Jones said:
>>The motion through the tunnel is not uniform accelerated.

Isaac Newton said it was.
He did not. Maybe you misunderstood him.

Eric M. Jones said:
>>Write the force acting on the falling body as a function of distance from the center, to see this.

Okay F=ma. Gravity is considered to be simply a point in the center of the sphere.
Yes, but F is not a constant for the motion through the tunnel.
Eric M. Jones said:
>>And for the orbital motion you should use the equations for circular motion.

The circular motion or the elliptical motion have the same formula, and the same orbital time

Eric
So why don't you use it then and get the correct value for the period?
I wrote you that the motion through the tunnel and around the circular path have the same period. Unfortunately, none of them is 76 minutes.
I don't know what formula are you using.

Eric M. Jones said:
Clever guy that I am, I am writing a small paper on Celestial Mechanics...simplified...really really simplified.
Albert Einstein is widely quoted as saying:
"Everything should be made as simple as possible, but not simpler." (or variants of the same idea)
You may have simplified a little too much.:biggrin:
 
Last edited:
  • #10
With the approximation of a uniform density of earth, the time would be the same.
However, real Earth has a variable density - the acceleration inside is higher than a linear formula would give, and objects falling through Earth would be a bit quicker than objects in an orbit.

BTW: I suspect any minimum energy subway tunnel of hypocycloidal shape has 1/2 the transit time of the watermelon, or 38 minutes, or 76 minutes round trip. A hypocycloid where the generating circle diameter is the same as the base circle radius generates a straight line through the center.
No - with the approximation of a uniform density of earth, every straight line has the same transit time (about 42 minutes). Other shapes (especially the shapes for the shortest transit time) can have shorter transit times.
 
  • #11
Thanks all for making me smarter.

Eric
 
  • #12
probably not very scientific here but, if you consider that gravity's force is centered on the center of the Earth, then the closer to center the faster you accelerate. you would have to accelerate fast enough to overcome the force that you obtained in that process. But when you start to reach the other side (away from the source) you are gravitating away from the source, which would mean that whatever energy you acquired, you will now be using to produce an "escape velocity". So, the equation from the entrance side, should measure enough energy to balance the exit side. Should equal zero, unless an outside force acts on the object. Unless the force of gravity is different depending on where you are on the Earth. Or altitude, depth, things like that. I'm just a student in this at this time, just a thought.
 
  • #13
october said:
probably not very scientific here but, if you consider that gravity's force is centered on the center of the Earth, then the closer to center the faster you accelerate.
Not if you are inside the Earth. For homogenous Earth the acceleration will decrease as you approach the center.
Even for actual (non-homogenous) Earth, as you go deep enough the acceleration deceases.
 

Related to Minimum Satellite Period problem

1. What is the Minimum Satellite Period problem?

The Minimum Satellite Period problem is a mathematical problem that involves determining the shortest possible time for a satellite to complete one orbit around a given planet or celestial body. It takes into account factors such as the gravitational pull of the planet, the satellite's distance from the planet, and its orbital velocity.

2. Why is the Minimum Satellite Period problem important?

The Minimum Satellite Period problem is important because it helps engineers and scientists calculate the minimum requirements for a satellite's orbit. This is crucial for satellite missions and communication systems, as the satellite's orbit must be carefully planned to ensure proper functioning and longevity.

3. How is the Minimum Satellite Period problem solved?

The Minimum Satellite Period problem is solved using mathematical formulas and equations that take into account the relevant factors such as the satellite's distance from the planet, the planet's gravitational force, and the satellite's speed and direction. Advanced computer programs are often used to solve this problem accurately.

4. What are some real-world applications of the Minimum Satellite Period problem?

The Minimum Satellite Period problem has many real-world applications in the field of satellite engineering and space exploration. It is used to plan and design satellite orbits for communication, weather monitoring, and navigation systems. It is also used for space missions to other planets, as well as for the placement of space stations and telescopes in Earth's orbit.

5. What challenges exist in solving the Minimum Satellite Period problem?

Solving the Minimum Satellite Period problem can be challenging due to the complex mathematical equations involved and the many variables that must be taken into account. Additionally, factors such as atmospheric drag and the gravitational pull of other celestial bodies can affect a satellite's orbit, making it difficult to determine the exact minimum period. Advances in technology and computing power have helped to overcome some of these challenges.

Similar threads

  • Astronomy and Astrophysics
Replies
5
Views
2K
  • Introductory Physics Homework Help
Replies
2
Views
2K
  • Introductory Physics Homework Help
Replies
1
Views
3K
  • Introductory Physics Homework Help
Replies
8
Views
1K
  • Introductory Physics Homework Help
Replies
10
Views
3K
  • Astronomy and Astrophysics
Replies
2
Views
4K
  • Astronomy and Astrophysics
Replies
10
Views
2K
  • Sci-Fi Writing and World Building
3
Replies
87
Views
5K
  • Introductory Physics Homework Help
Replies
7
Views
3K
  • Introductory Physics Homework Help
Replies
4
Views
2K
Back
Top