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!mhuxr!mhuxn!ihnp4!ucbvax!space From: J.JPM@LOTS-B (Jim McGrath) Newsgroups: net.space Subject: The Bootstrap Problem Message-ID: <12173196004.103.J.JPM@LOTS-B> Date: Mon, 6-Jan-86 20:22:49 EST Article-I.D.: LOTS-B.12173196004.103.J.JPM Posted: Mon Jan 6 20:22:49 1986 Date-Received: Wed, 8-Jan-86 06:05:30 EST Sender: daemon@ucbvax.BERKELEY.EDU Organization: The ARPA Internet Lines: 26 As much as I like to play with concepts such as 200 km long accelerators in orbit to boost sub-orbital payloads to low earth orbit, these proposals have usually left me with an empty feeling. The problem is that in order to construct such a large structure in space, you already have to have a good space transportation system. In other words, how do we get there from here? What do people think of the prospects of placing a SMALL accelerator into orbit, and using it to give a velocity boost to payloads coming from earth? This would still require some form of earth based accelerator system or the like, but over time you could, by building more orbital accelerators, reduce the velocity that needs to be imparted on earth. This would allow you to build more, cheaper earth based accelerators, and thus a positive feedback would begin. The question is, what is the maximum size (in length and acceleration) of an orbital accelerator that we could reasonaby construct using Shuttle or immediate post-Shuttle systems? And what is the biggest earth based accelerator/launch system that we could construct? Finally, can the first impart enough velocity to the second to make orbital velocity? Jim -------