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Astronomical Observations & Research


Earth's first ring system! Would a Saturn-like ring system around planet Earth remain stable?
[An astronomical paper by A. Ahad]

Copyright © 2004 Abdul Ahad. All rights reserved.

Article posted: 9 October 2004



Abstract

Future orbital engineering projects, such as the construction of space stations and orbital colonies, may result in unwanted debris accumulating in a ring formation around the Earth. To enable safe passage of interplanetary and lunar spacecraft to and from the Earth, it would be highly desirable to contain the ring particles from such projects in a neat plane so that they do not randomly scatter around the planet over time and pose a hazard to spaceflight. This paper illustrates that such a ring system around the Earth is unlikely to remain stable over any length of time and the degree and pace of scatter of ring material is a function of the orbital ellipticity and inclination of such a ring system.




Dynamical models have shown that the orbit of a particle circling around the Earth will precess (rotate) its line of nodes along the equator over time according to the equation [1]:-

-3/2 * J2 * (R^2 / p^2) * n * cos (i) . . . . . . . . . . . . . . . . . . .(1)

[where J2 is a constant related to Earth's flattening (about 0.001), R is the radius of the Earth (about 6378km), p is the "parameter" of the orbit (= a*(1-e^2)), n is the mean motion of the orbit (=sqrt(mu/a^3)), and i is the inclination. (And "a" is the semimajor axis of the orbit, equal to its radius for a circular orbit, "e" is the eccentricity, 0 for a circular orbit, and "mu" is about 398600km^3/s^2, Earth's mass times the universal gravitational constant.) The result is in radians per second if you've been consistent with the other units.]

In addition, a first order approximation for the in-plane rotation of the orbit (i.e. the "line of apsides") is given by:-

3/2 * J2 * (R^2 / p^2) * n * (2 - 5/2 * sin^2 i) . . . . . . . . . . .(2)

The orbit precessions described by these equations are due to uneven mass (and gravity) distribution of an oblate [2] Earth. Based on the *first order* dynamical model underlying the above equations, three seprate ring orientations are considered here to identify if an optimum solution exists for achieving dynamical stability of such a ring system.


Case 1 - Circular ring system, inclined to equator

In figure 1 below, consider a perfectly concentric, circular ring system inclined at an angle i-degrees relative to the Earth's equatorial plane, whose boundaries are marked by two ring particles P1 and P2 orbiting at the outer and inner edges of the ring, respectively (the purple ring). At time t1, the particles are at positions P1-1 and P2-1, relative to a common longitude of ascending node omega-1 as shown. Now, by equation (1) above we expect the ascending nodes of the two particles to precess at slightly different rates, depending on the distance separating them. At some future epoch, t2, we expect the particles to be at P1-2 and P2-2 relative to their new separate longitudes of ascending nodes. From this illustration, it can be seen that the new ring formation (blue) is no longer concentric and the two particles have scattered away from the original (purple) ring formation.

Figure 1 [Image - Abdul Ahad]

By equations (1) and (2) above, there is one unique case where a ring system *could* theoretically hold stable: where the inclination, i=90 degrees (exactly polar) and the eccentricity, e=0 (exactly circular). That orientation would however cause the ring plane to experience maximum solar light pressure (if oriented face on relative to the Sun) and the stipulation here is based on only a *first order* dynamical model that ignores perturbative influences from the Sun and the Moon.


Case 2 - Circular ring system, in equatorial plane

This scenario is illustrated below, by figures 2(a) and 2(b), where since the ring system is perfectly circular (the line of *apsides* for every constituent particle is undefined) and precisely co-planer with the Earth's equatorial plane (the line of *nodes* for every constituent particle is undefined), the differential rates of precession between individual particles within the ring system stipulated by dynamical equations (1) and (2) will not affect its overall shape and stability.

Figure 2a [Image - Abdul Ahad]

Figure 2b [Image - Abdul Ahad]




Case 3 - Elliptical ring system in equatorial plane

In this scenario, illustrated in figure 3 below, the in-plane precession component stipulated by equation (2) above will be the determinant factor that causes the non-circular ring system to scatter its constituent particles over time.

Figure 3 [Image - Abdul Ahad]



External Forces

From a *first order* dynamical model's perspective, one would conclude that a perfectly spherical, co-planer set of rings orbiting at a decay-immune altitude of say 40,000 km above the equator ought to remain fully stable over time (as depicted in case [2] above).

However, studies of the behaviour of geostationary satellites, whose thrusters for station-keeping duties had exhausted, have shown [3] that the perturbing influences of the Sun and the Moon cause these satellites to drift within a belt of approximately +/- 15 degrees geocentric latitude either side of the equator with an oscillation period of roughly 50 years. This is due to a combined precessional effect between the Sun's perturbing influence (running along the ecliptic plane whose inclination is 23.4 degrees relative to the Earth's equatorial plane) and the Moon's perturbing influence (running along its orbital plane which is inclined at 5.1 degrees relative to the ecliptic plane). In actual fact, the satellite orbits oscillate around the Laplacian plane of the Earth-Moon system, which runs between the ecliptic and equatorial planes and is inclined at an angle of 7.5 degrees to the Earth's equator with an intersection along the line of equinoxes.

Figure 4a [Image - Abdul Ahad]

Figure 4b [Image - Abdul Ahad]



Thus the combined perturbing influences of the Sun and the Moon together would cause ring particles even in the apparently most stable orientation [case (2) above] to scatter over many years into a belt of +/- 15 degrees around the equator (7.5 degrees relative to the Laplacian plane, which itself is inclined at 7.5 degrees and precessing relative to the Earth's equatorial plane).

In conclusion, maintaining a dynamically stable ring system around the Earth is not possible in virtually all orientations owing to the complex interactive forces at play between the Earth, the Moon and the Sun.

However.... some experts appear to suggest that such a ring could have existed for hundreds of thousands of years, causing climatic effects on the Earth, as revealed here [4] and here.

This article was featured in the following links and discussion forums:-

Google Earth's "Flyin' Globe" (See URL in the section headed 'Links Corner')
Google Earth Community (See URL in the section headed 'Lord of Rings...' Here is a scientist who says that it�s impossible to build. And he says why.)
Virtually Strange - UFO site (Visit the second URL listed on that page)

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My original discussion articles on this topic!

AA Institute of Space Science & Technology



R E F E R E N C E S

[1] From the usenet thread "Precession of polar satellites" as supplied by Henry Spencer on sci.space.tech, 2003-11-07. Originally from A.E. Roy's "Orbital Motion", 3rd ed.
[2] "Variations in the Earth's oblateness during the past 28 years" - JOURNAL OF GEOPHYSICAL RESEARCH, VOL. 109, B09402 2004-09-16
[3] "A Geosynchronous Orbit Search Strategy" - Africano J.; Schildknecht T.; Matney M.; Kervin P.; Stansbery E.; Flury W. , 2000-01-01
[4] News article "Rings around the Earth: A clue to climate change?" - Peter J. Fawcett, of the University of New Mexico, and Mark B.E. Boslough, of the U.S. Department of Energy�s Sandia National Laboratories. , 2002-09-11



Copyright © 2004 by Abdul Ahad. All rights reserved.


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