Relay-Version: version B 2.10 5/3/83; site utzoo.UUCP Path: utzoo!mnetor!uunet!husc6!cmcl2!rutgers!bellcore!faline!karn From: karn@faline.bellcore.com (Phil R. Karn) Newsgroups: sci.space.shuttle Subject: Re: Throttling the Challenger Message-ID: <1482@faline.bellcore.com> Date: Fri, 16-Oct-87 21:50:30 EDT Article-I.D.: faline.1482 Posted: Fri Oct 16 21:50:30 1987 Date-Received: Sun, 18-Oct-87 05:44:47 EDT References: <340@ablnc.ATT.COM> Organization: Bell Communications Research, Inc Lines: 21 Keywords: Challenger Throttle Summary: throttle control is normal and automatic During a normal launch the crew does little more than watch the displays and twiddle their thumbs; all engine control (gimbaling, throttling, etc) is completely under onboard computer control. Control of a launch vehicle is something that humans do very badly but computers do extremely well, so there's no practical alternative. The crew has the ability to take manual control, but that is little more than a last-ditch backup. Even aborts are done under computer control, at least as long as engines are firing. The "callouts" you hear during a launch are simply confirmations of events that happen automatically; no one is pushing any buttons. The reduction of engine throttle during the first minute of flight is programmed in to reduce the stresses on the launcher as it hits "Max-Q", the region of maximum aerodynamic pressure. Once altitude has increased sufficiently the throttle may again be increased because the less dense atmosphere no longer generates enough drag to worry about. The SRBs are also "throttled back" during this time, but this is not under control of the onboard computers; their thrust-vs-time curves are established by the way propellant is loaded into them. Phil