Relay-Version: version B 2.10 5/3/83; site utzoo.UUCP Posting-Version: version B 2.10.3 4.3bsd-beta 6/6/85; site ucbvax.BERKELEY.EDU Path: utzoo!watmath!clyde!burl!ulysses!ucbvax!space From: KFL@MC.LCS.MIT.EDU ("Keith F. Lynch") Newsgroups: net.space Subject: Ulysses probe Message-ID: <[MC.LCS.MIT.EDU].836296.860303.KFL> Date: Mon, 3-Mar-86 02:05:00 EST Article-I.D.: <[MC.LCS.MIT.EDU].836296.860303.KFL> Posted: Mon Mar 3 02:05:00 1986 Date-Received: Tue, 4-Mar-86 01:56:05 EST Sender: daemon@ucbvax.BERKELEY.EDU Organization: The ARPA Internet Lines: 21 From: brahms!desj@ucbvax.berkeley.edu (David desJardins) I don't have any idea what these people are talking about. The whole idea is that Ulysses is being launched to rendezvous with Jupiter just like Voyager and Galileo, but it will swing around Jupiter and back over the solar pole. Presumably it will then leave the solar system; what would cause it to circle around to the other pole?? I just spent several hours working out the math, and I am somewhat confused. I assume that unlike the Voyager and Pioneer probes, that Ulysses has some onboard fuel to be used in the vicinity of Jupiter. If the Jupiter pass is completely passive, as with Pioneer and Voyager, the furthest out of the ecliptic it could get would be 26 degrees, not 90 degrees as would be necessary to go over either of the Sun's poles. I have proven to my satisfaction that the orbit does not escape from the solar system but will continue to pass over both poles if it passes over one. Can someone from JPL or NASA give us the facts? ...Keith