Relay-Version: version B 2.10 5/3/83; site utzoo.UUCP Path: utzoo!watmath!clyde!burl!ulysses!gamma!epsilon!zeta!sabre!petrus!bellcore!decvax!genrad!panda!talcott!harvard!seismo!hao!nbires!boulder!cisden!lmc From: lmc@cisden.UUCP (Lyle McElhaney) Newsgroups: net.columbia Subject: Re: SRB vs liquid Message-ID: <497@cisden.UUCP> Date: Sun, 9-Feb-86 00:40:38 EST Article-I.D.: cisden.497 Posted: Sun Feb 9 00:40:38 1986 Date-Received: Wed, 12-Feb-86 20:57:12 EST References: <615@uwvax.UUCP> <3045@umcp-cs.UUCP> <471@ecn-pc.UUCP> Organization: ConTel Information Systems, Denver Lines: 19 > What exactly is the configuration of Ariane? I keep hearing that one > of the stages is solid fueled, but a drawing printed in the Chicago > Tribune shows three stages, all liquid fueled. > It has three liquid-fuelled stages. The first two stages use hypergolic fuels, the third uses H2/O2 cryogenics. > Additionally, is there anything new and novel about the Ariane? From > what I have been able to gather, it seems to be pretty mundane rocket. > It's major advantage seems to be that it is launched fairly near the > equator, and can put satellites out at GEO distances from the Earth. Nothing novel; just good reliable technology. It can place 1700 Kg at geosync, 4800 Kg at LEO, and 2500 Kg in Sun-synchronous orbit. The shuttle can place 29,500 Kg in LOE. Cost, of course, is another matter, as is launch availability, especially now. Lyle McElhaney ...hao!cisden!lmc