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!ucbvax!space From: dietz@SLB-DOLL.CSNET (Paul Dietz) Newsgroups: net.space Subject: Phobos to Earth Via Skyhook Message-ID: <8601071449.AA14192@s1-b.arpa> Date: Tue, 7-Jan-86 08:56:40 EST Article-I.D.: s1-b.8601071449.AA14192 Posted: Tue Jan 7 08:56:40 1986 Date-Received: Wed, 8-Jan-86 23:43:07 EST Sender: daemon@ucbvax.BERKELEY.EDU Organization: The ARPA Internet Lines: 14 Using the data on Kevlar and on Phobos's orbit, I got the following numbers: a 3000 km long kevlar cable stretched out from Phobos will accelerate payloads to ~ 1 km/sec after escape from Mars's gravity well. Even with a safety factor of 2, the cable will have a taper of less than 2:1. A cable 7500 km long will accelerate payloads to 3.1 km/sec after escape, and will have a taper of 25:1 with a safety factor of two. Injection into a Hohmann orbit from Mars to Earth would require 2.63 km/sec velocity change if Mars and Earth were in circular orbits and in the correct positions (they aren't, but I'll ignore that). However, such an injection would require a velocity change nearly parallel to the ecliptic; Phobos's orbit is inclined 25 degrees. The direction of the orbit can be modified by throwing the payload into a Mars intersecting orbit and using the subsequent encounter to fix the orbit's inclination.