Relay-Version: version B 2.10 5/3/83; site utzoo.UUCP Posting-Version: version B 2.10.1 6/24/83; site ttidcb.UUCP Path: utzoo!linus!philabs!ttidca!ttidcb!jackson From: jackson@ttidcb.UUCP (Dick Jackson) Newsgroups: net.space Subject: Manned Mars Trip Message-ID: <565@ttidcb.UUCP> Date: Thu, 5-Dec-85 14:46:09 EST Article-I.D.: ttidcb.565 Posted: Thu Dec 5 14:46:09 1985 Date-Received: Sat, 7-Dec-85 16:21:01 EST Organization: TTI, Santa Monica, CA. Lines: 24 There's talk about an international manned Mars expedition. Naturally I'm all for it. Is there a generally agreed best way to go? My very uninformed thoughts are: - A very modular spacecraft, for redundancy - Artificial gravity through spinning - Return booster sent separately to Mars orbit My spaceship, assembled in EO of course, would have at least three manned modules plus landers which would fit together in a package for the acceleration phase. Once at cruise the manned units would be sent out on the end of tethers to form a sort of spider web, then the whole thing would be spun up. For entry into Mars orbit the thing would be pulled together again. Once in orbit, the manned units could possibly be sent off on diverse missions, e.g. rendezvous with the moons. I don't really care if this makes total sense, the main point is that system design for the Mars mission seems to offer a very rich field for innovative spacefaring ideas. Who's next? Dick Jackson