Maintaining orbit around the moon

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    Moon Orbit
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Discussion Overview

The discussion revolves around the dynamics of maintaining an orbit around the Moon, exploring the effects of gravitational forces, orbital stability, and the implications of different orbital parameters. Participants examine theoretical and practical aspects of lunar orbits, including the influence of Earth's gravity and the characteristics of low lunar orbits.

Discussion Character

  • Exploratory
  • Technical explanation
  • Debate/contested
  • Mathematical reasoning

Main Points Raised

  • Some participants propose that any object orbiting the Moon may experience increasing elliptical orbits leading to a potential crash into the Moon, questioning the duration of such effects.
  • It is noted that low orbit times are proportional to the square root of the average density, with estimates suggesting approximately 105 minutes for very low lunar orbits.
  • Concerns are raised about the influence of Earth's gravity on lunar orbits, with speculation on how long this effect might persist.
  • One participant suggests that spacecraft in low lunar orbits are likely dominated by the Moon's gravity, similar to how the Moon orbits Earth.
  • Another participant discusses the stability of orbits around the Moon, indicating that while Earth affects these orbits, they can remain stable at lower altitudes, specifically below 20,000 to 30,000 km.
  • There is a mention of the gravitational forces from the Sun affecting the Moon, which some argue does not negate the stability of the Moon's orbit over billions of years.
  • A thought experiment is introduced regarding the potential tidal effects on the Moon if it had oceans and a 24-hour rotation period, leading to a discussion on the relationship between mass and tidal forces.
  • One participant highlights that stable circular lunar orbits exist below an inclination of 39.6º but may not be suitable for polar exploration due to their equatorial proximity.
  • Concerns are raised about the instability of polar orbits for exploration purposes.

Areas of Agreement / Disagreement

Participants express multiple competing views regarding the stability and dynamics of lunar orbits, with no consensus reached on the implications of Earth's gravitational influence or the characteristics of stable orbits.

Contextual Notes

Participants acknowledge limitations related to the assumptions made about gravitational effects, the definitions of stable orbits, and the conditions under which orbits may become unstable, particularly concerning mass concentrations on the Moon.

vjk2
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http://news.discovery.com/space/ast...s-put-an-asteroid-into-lunar-orbit-130111.htm

Basically, wouldn't any object that orbited around the moon gradually see its orbit be made more and more eliptical until it crashed into the moon itself?

Also, it actually takes longer for a satellite to orbit around the moon than the Earth itself, due to the Earth being more dense despite having a much larger diameter, correct?
 
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vjk2 said:
Basically, wouldn't any object that orbited around the moon gradually see its orbit be made more and more eliptical until it crashed into the moon itself?
Why do you expect this?

Low orbit times are proportional to ##\sqrt{\rho}## with the average density ρ only. This gives ~105 minutes for very low lunar orbits.
 
mfb said:
Why do you expect this?

Low orbit times are proportional to ##\sqrt{\rho}## with the average density ρ only. This gives ~105 minutes for very low lunar orbits.

Earth gravity should gradually affect any object orbiting. I wonder for how long thought.

It takes 90 minutes for the space shuttle to orbit the Earth.
 
vjk2 said:
Earth gravity should gradually affect any object orbiting. I wonder for how long thought.

It takes 90 minutes for the space shuttle to orbit the Earth.

I think the spacecraft is well within the distance that the effect of the moon's gravity dominates over the effect of the Earth's. But another way to think about it is that the object is in a stable orbit around Earth just like the moon is.
 
I took 82 minutes, which would correspond to a height of 0 km (not possible as Earth has an atmosphere, of course).

Earth affects the orbit, but orbits which are not too high can be stable for a long time - a satellite around the moon should be closer than 20 000 to 30 000km.
Consider the earth-moon-system as interesting example: The gravitational force between moon and sun exceeds the gravitational force between moon and earth! But still, the lunar orbit has been stable for some billion years.
 
cepheid said:
I think the spacecraft is well within the distance that the effect of the moon's gravity dominates over the effect of the Earth's. But another way to think about it is that the object is in a stable orbit around Earth just like the moon is.

It should be akin to how the moon affects tides on the earth. As a thought experiment...if the moon had oceans, and if it rotated instead of being tidally locked, would the "tides" be greater than the Earth's tides, due to the mass of the Earth being so great compared to the mass of the moon vs the earth?
 
With an earth-like ocean and 24-hours rotation period, moon would have larger tides.
This has nothing to do with an orbit, however.
 
mfb said:
I took 82 minutes, which would correspond to a height of 0 km (not possible as Earth has an atmosphere, of course).

Earth affects the orbit, but orbits which are not too high can be stable for a long time - a satellite around the moon should be closer than 20 000 to 30 000km.

The maximum altitude seems to be much lower for circular orbits

http://science.nasa.gov/science-news/science-at-nasa/2006/30nov_highorbit/

And low orbits can also be unstable, because of mass concentrations in the moon

http://science.nasa.gov/science-news/science-at-nasa/2006/06nov_loworbit/
 
Inclination is the problem here:
NASA said:
Stable circular lunar orbits do exist below an inclination of 39.6º, says Ely, but they spend so much time near the equator that "they are terrible orbits for covering the poles."
[...]
The instability of polar orbits poses a real problem for exploration.
 

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