Path: utzoo!mnetor!uunet!portal!cup.portal.com!CaptainDave
From: CaptainDave@cup.portal.com
Newsgroups: sci.space.shuttle
Subject: Re: General Question
Message-ID: <2954@cup.portal.com>
Date: 5 Feb 88 00:01:20 GMT
References: <3a106850.7011@apollo.uucp>
Organization: The Portal System (TM)
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XPortal-User-Id: 1.1001.2255


Just a quick question to anyone who might have an answer.
What is the thrust distribution in percent between the two SRBs
and the shuttle's three engnes at the time they are all operating
at maximum thrust. I know the shuttle can continue its launch
with only two engines operating. I am only interested in percents
but if you have the thrust values handy, I am sure others would be interested.