Relay-Version: version B 2.10 5/3/83; site utzoo.UUCP Path: utzoo!watmath!clyde!cbatt!ihnp4!houxm!mhuxt!mhuxr!ulysses!bellcore!petrus!ka9q!karn From: karn@ka9q.bellcore.com (Phil Karn) Newsgroups: sci.space Subject: Re: Comsat fuel saving maneuver invented Message-ID: <183@ka9q.bellcore.com> Date: Sun, 19-Oct-86 19:53:43 EDT Article-I.D.: ka9q.183 Posted: Sun Oct 19 19:53:43 1986 Date-Received: Tue, 21-Oct-86 23:12:45 EDT References: <8610180704.AA03474@s1-b.arpa> Organization: Home for Burned-out Hackers Lines: 24 > The NY Times reported today (10/16) that engineers at Comsat Corp. > have developed a technique for reducing the fuel consumption > of comsats by up to 90%. The technique can be applied remotely to > satellite already in orbit. I'm puzzled by this move on the part of Comsat. It has been well known for many, many years that North/South stationkeeping is much more expensive in terms of fuel consumption than East/West stationkeeping, and that a satellite that foregoes N/S thrusting will describe a "figure 8" orbit whose inclination varies cyclically with time due to lunar and solar perturbations. However, they're claiming that this is a new, novel and PATENTABLE idea. I hope there's something more to it than I've heard so far, since AMSAT has been saying (in print) for several years now that we would only do E/W stationkeeping on our Phase 4 amateur birds in order to minimize hydrazine requirements. The only problem I can see with this technique is how they are going to keep the antenna footprint in a fixed position given a spinning spacecraft. I guess they could reorient the spin axis so that it's always normal to the orbit plane. This would cause a 24-hour cycle in which the footprint would "rotate" at the equator crossings. With a three-axis stabilized (i.e., non-rotating) spacecraft, however, this could be avoided. Phil