Relay-Version: version B 2.10 5/3/83; site utzoo.UUCP Path: utzoo!watmath!clyde!burl!ulysses!mhuxr!mhuxt!houxm!whuxl!whuxlm!akgua!gatech!seismo!mcvax!ukc!csw From: csw@ukc.UUCP Newsgroups: net.wanted,net.space,net.columbia Subject: Shuttle Payload Assist Modules Message-ID: <662@eagle.ukc.ac.uk> Date: Fri, 31-Jan-86 09:11:55 EST Article-I.D.: eagle.662 Posted: Fri Jan 31 09:11:55 1986 Date-Received: Sun, 2-Feb-86 01:02:07 EST Organization: U of Kent at Canterbury, Canterbury, UK Lines: 19 Xref: watmath net.wanted:8059 net.space:5480 net.columbia:1914 I am looking for details on space shuttle payload assist modules. Basically I need details of PAM dry mass Propellant mass Average vaccum thrust Burn time etc. i.e. slightly more info than they usually give in A&STW, JBIS, Spacefight etc. If anyone out there has this data, or could point me in the direction of the right reference, I would be very happy. Doing literature searches can be very boring at times. Thanks in advance, Chris Welch csw@ukc.uucp Cranfield Institute U.K.