AA Institute
Oct11-04, 03:52 AM
<jabberwocky><div class="vbmenu_control"><a href="jabberwocky:;" onClick="newWindow=window.open('','usenetCode','toolbar=no, location=no,scrollbars=yes,resizable=yes,status=no ,width=650,height=400'); newWindow.document.write('<HTML><HEAD><TITLE>Usenet ASCII</TITLE></HEAD><BODY topmargin=0 leftmargin=0 BGCOLOR=#F1F1F1><table border=0 width=625><td bgcolor=midnightblue><font color=#F1F1F1>This Usenet message\'s original ASCII form: </font></td></tr><tr><td width=449><br><br><font face=courier><UL><PRE>\n\nSuppose an asteroid by a distant future engineering achievement has\nbeen captured into orbit around the Earth.\nNow suppose we want to carve it out by detonating a series of missiles\nthat incrementally hollow their way into the body of such an asteroid.\nThe material excavated out of the body would create a thin ring system\naround the Earth, as I try to illustrate here:-\n\nhttp://uk.geocities.com/aa_spaceagent/restricted/earth-ring.html\n\nMy main concern with such a project is one of SAFETY. I\'d like to know\nwhat a *safe* perigee (minimum) altitude would be necessary to prevent\norbital decay of ring material. I don\'t want any material from my\nhypothetical ring system coming down toward the Earth under any\ncircumstances. Would the ring material be contained in a narrow plane\nof fixed orbital incline, or would it scatter over time?\n\nQUESTION: I am under pressure to demonstrate by way of a mathematical\nmodel the dynamical stability of such a ring system, composed of small\nparticles being gravitationally influenced by the Earth and the Moon\nby way of "3 body problem".\n\nWhat are the analytical equations necessary to help demonstrate\n*theoretically* that such ring particles would indeed be stable in\ntheir orbital paths around the Earth? Or if not, how would I be able\nto show this?\n\nI would sincerely appreciate all help, as this is quite *pivotal* to\nmy research on this article.\n\nThanks for any support.\nAbdul Ahad\n</UL></PRE></font></td></tr></table></BODY><HTML>');"> <IMG SRC=/images/buttons/ip.gif BORDER=0 ALIGN=CENTER ALT="View this Usenet post in original ASCII form"> View this Usenet post in original ASCII form </a></div><P></jabberwocky>Suppose an asteroid by a distant future engineering achievement has
been captured into orbit around the Earth.
Now suppose we want to carve it out by detonating a series of missiles
that incrementally hollow their way into the body of such an asteroid.
The material excavated out of the body would create a thin ring system
around the Earth, as I try to illustrate here:-
http://uk.geocities.com/aa_spaceagent/restricted/earth-ring.html
My main concern with such a project is one of SAFETY. I'd like to know
what a *safe* perigee (minimum) altitude would be necessary to prevent
orbital decay of ring material. I don't want any material from my
hypothetical ring system coming down toward the Earth under any
circumstances. Would the ring material be contained in a narrow plane
of fixed orbital incline, or would it scatter over time?
QUESTION: I am under pressure to demonstrate by way of a mathematical
model the dynamical stability of such a ring system, composed of small
particles being gravitationally influenced by the Earth and the Moon
by way of "3 body problem".
What are the analytical equations necessary to help demonstrate
*theoretically* that such ring particles would indeed be stable in
their orbital paths around the Earth? Or if not, how would I be able
to show this?
I would sincerely appreciate all help, as this is quite *pivotal* to
my research on this article.
Thanks for any support.
Abdul Ahad
been captured into orbit around the Earth.
Now suppose we want to carve it out by detonating a series of missiles
that incrementally hollow their way into the body of such an asteroid.
The material excavated out of the body would create a thin ring system
around the Earth, as I try to illustrate here:-
http://uk.geocities.com/aa_spaceagent/restricted/earth-ring.html
My main concern with such a project is one of SAFETY. I'd like to know
what a *safe* perigee (minimum) altitude would be necessary to prevent
orbital decay of ring material. I don't want any material from my
hypothetical ring system coming down toward the Earth under any
circumstances. Would the ring material be contained in a narrow plane
of fixed orbital incline, or would it scatter over time?
QUESTION: I am under pressure to demonstrate by way of a mathematical
model the dynamical stability of such a ring system, composed of small
particles being gravitationally influenced by the Earth and the Moon
by way of "3 body problem".
What are the analytical equations necessary to help demonstrate
*theoretically* that such ring particles would indeed be stable in
their orbital paths around the Earth? Or if not, how would I be able
to show this?
I would sincerely appreciate all help, as this is quite *pivotal* to
my research on this article.
Thanks for any support.
Abdul Ahad