Relay-Version: version B 2.10 5/3/83; site utzoo.UUCP Posting-Version: version B 2.10.1 6/24/83; site ssc-vax.UUCP Path: utzoo!linus!security!genrad!grkermit!masscomp!clyde!floyd!vax135!cornell!uw-beaver!ssc-vax!eder From: eder@ssc-vax.UUCP Newsgroups: net.space Subject: Re: Lunar landings, cold mining, launchings Message-ID: <755@ssc-vax.UUCP> Date: Mon, 16-Jan-84 15:25:55 EST Article-I.D.: ssc-vax.755 Posted: Mon Jan 16 15:25:55 1984 Date-Received: Fri, 20-Jan-84 01:12:54 EST References: <15313@sri-arpa.UUCP> Organization: Boeing Aerospace, Seattle Lines: 22 From Dani Eder at Boeing Aerospace 16 January 1984 Another method of getting stuff to and from the lunar surface is a rotating cable. Since the Moon is much smaller than the Earth, material strengths can be lower for cable type systems. For example, suppose you have a cable orbiting the Moon at 1650 meters/sec. It is spinning so that it's outer tip is moving at lunar escape velocity (2333 meters/sec), and its inner tip is moving at a corresponding amount slower(966 meters/ sec). On your way from Earth, you come in at escape velocity, grab on for half a rotation of the cable, then let go. You have reduced your velocity from 2333 meters/sec to 966 meters/ sec. You do the rest with rockets. Compared with pure rockets, you have to do only 41% as much velocity change. If you are using LOX-Hydrogen rockets your fuel use goes from .677 times landed weight to .239 times landed weight, only 35% as much fuel. You don't have to have any special facility on the lunar surface. On the way up, you drop off some oxygen or aluminum to feed an ion thruster or mass driver at the center of the cable. This is required to balance any net momentum change if the payload to the moon does not equal the payload from the moon.