Relay-Version: version B 2.10 5/3/83; site utzoo.UUCP Posting-Version: version B 2.10 5/3/83; site utzoo.UUCP Path: utzoo!henry From: henry@utzoo.UUCP (Henry Spencer) Newsgroups: net.space Subject: Re: Galileo mission to Jupiter Message-ID: <5592@utzoo.UUCP> Date: Sun, 12-May-85 01:16:05 EDT Article-I.D.: utzoo.5592 Posted: Sun May 12 01:16:05 1985 Date-Received: Sun, 12-May-85 01:16:05 EDT References: <1671@mordor.UUCP> <24@escher.UUCP>, <10563@brl-tgr.ARPA> Organization: U of Toronto Zoology Lines: 64 > Ok, I've heard lots of times about the 'gravity assist' > maneuver used to sometimes dramatically increase the speed of > a spacecraft by flying close to a bigger mass. Now the question > is, how does this work? I understand that you would gain energy > by dropping weight when inside a gravity well (and having the > velocity vector pointed so that you could make it out, now lighter > and requiring less energy), but is that the ONLY cause of the > acceleration? I thought that this effect was also due to rotating > the velocity vector of the spacecraft. There are two separate types of maneuver here. One, classically called a "gravity-well" maneuver, flies very close to a large mass so that an engine burn can be made at the lowest possible potential energy. The other, often called a "gravity-boost" maneuver, is a three-body maneuver (the Sun is usually the third body) using gravity alone to transfer some momentum from a large body to the spacecraft. The gravity-well maneuver exploits the difference between momentum and kinetic energy to give the spacecraft higher final velocity. How much velocity you gain from an engine burn is a matter of momentum; how much you gain or lose to a gravity field is a matter of energy. Since energy is proportional to the *square* of velocity, and leaving a gravity field subtracts a fixed amount of energy, the higher the velocity with which you start to leave a gravity field, the less velocity you lose to gravity. So an engine burn's effect is magnified if you fly into a handy gravity field before making it. The scales remain balanced: you carry the fuel down with you and don't bring it back up, so it loses energy. The gravity-boost maneuver exploits relative motions. With respect to Jupiter, flying past Jupiter will only rotate your velocity vector, and cannot change its magnitude. The key is the words "with respect to Jupiter". If what you care about is velocity with respect to something else, and Jupiter is moving with respect to that something else, then you can gain or lose velocity. In the limiting case, an extremely tight hyperbola whips you around an almost 180-degree turn with respect to Jupiter. You leave heading almost exactly back along your approach path. So Jupiter-relative Vdepart = -Vapproach. If your approach was, say, along Jupiter's orbit in the reverse direction, then viewed from the Sun you were moving at Vapproach-Vjupiter on the way in, and on the way out you're at Vdepart-Vjupiter = -Vapproach-Vjupiter = -(Vapproach+Vjupiter). So your Sun-relative velocity vector has been flipped 180 degrees (hence the minus sign), but has also had 2*Vjupiter added to it. There is nothing magic about it, since Jupiter has lost the same amount of Sun-relative momentum you've gained. But considering the relative masses, a given amount of momentum matters a lot more to you than to Jupiter! It is, of course, possible to combine the two effects. > I've also heard that the maneuver works best when you get > closest to the object being slingshot off of. Is this true? > (it would seem so) Both types of maneuver work best if you get as close as you can. The gravity-well maneuver works best if you convert as much potential energy as possible into kinetic energy first. The gravity-boost maneuver's results depend on how far your velocity vector rotates with respect to the body you're flying past; the closer the approach, the sharper the turn. Of course, you can only fly so close without hitting something. There was some interest in arranging Voyager 2's Neptune flyby to send it on to Pluto, but somebody calculated the approach distance and it came out to be several hundred kilometers *below* the cloud tops... -- Henry Spencer @ U of Toronto Zoology {allegra,ihnp4,linus,decvax}!utzoo!henry