Relay-Version: version B 2.10 5/3/83; site utzoo.UUCP Posting-Version: version B 2.10.2 9/18/84; site lanl.ARPA Path: utzoo!watmath!clyde!burl!ulysses!mhuxr!mhuxb!mhuxn!mhuxm!mhuxj!houxm!whuxlm!akgua!mcnc!philabs!cmcl2!lanl!jlg From: jlg@lanl.ARPA Newsgroups: net.space,net.astro Subject: Re: L5 Message-ID: <20164@lanl.ARPA> Date: Thu, 24-Jan-85 12:32:13 EST Article-I.D.: lanl.20164 Posted: Thu Jan 24 12:32:13 1985 Date-Received: Mon, 28-Jan-85 05:51:18 EST References: <79@drivax.UUCP> <356@ssc-vax.UUCP> Sender: newsreader@lanl.ARPA Distribution: net Organization: Los Alamos National Laboratory Lines: 16 Xref: watmath net.space:3536 net.astro:473 > I'll give it a try. A stable point is where there is no > acceleration relative to the Earth and Moon. This requires that > forces be balanced so there is no net force to produce an > acceleration. In the case of the L2 point this is easy to see, > since it is between the bodies, there is somewhere where the > attractions are equal and opposite. An equilibrium point is one where the forces ballance to zero. Such a point is not necessarily stable. A stable equilibrium point is one where a slight deviation from the correct location will not cause the unballanced forces to push you away from the equilibrium point. For orbital systems, L1, L2, and L3 are unstable equilibria and L4 and L5 are stable equilibria. This is why L4 and L5 are the locations most often proposed for space stations - they don't have to continuously expend propellant to keep their position against orbital purturbations.