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: acourt@BBN-VAX.ARPA ("Anthony J. Courtemanche") Newsgroups: net.space Subject: Shuttle Ditching Message-ID: <8602032227.AA10998@s1-b.arpa> Date: Mon, 3-Feb-86 16:45:00 EST Article-I.D.: s1-b.8602032227.AA10998 Posted: Mon Feb 3 16:45:00 1986 Date-Received: Wed, 5-Feb-86 05:02:22 EST Sender: usenet@ucbvax.BERKELEY.EDU Reply-To: ac%mit-oz@MIT-MC.ARPA Organization: The ARPA Internet Lines: 48 Although, as said earlier, it is doubtful whether the Shuttle could survive the deceleration of landing in the Atlantic, it is interesting to think about what the possible abort scenarios would entail. First, the media (& NASA photos) say that an abnormal plume eminated from the right SRB at least 15 seconds before the deadly external tank explosion. Is 15 seconds long enough to initiate an abort? At least three events would have to occur: 1) Ground crew interprets visual data, determines that the situation is deadly, and tells shuttle commander to abort. My guess is that this could take up a very significant part of 15 seconds. 2) Shuttle commander receives abort message and initiates abort sequence. I don't know how well the Shuttle pilots are trained to respond to such frightening news, but I would guess that the commander wouldn't freeze for more than say 0.5 seconds. Now as far as initiating the abort sequence, I've heard that this consists of pulling a lever and pressing a button. If this is true, I would guess that this could be done within a second. 3) Shuttle breaks away from external tank soon enough to survive the explosion. I have no idea how different the trajectories of the shuttle and the ET/SRB assembly can be made to be during an abort. I would guess that in any case, to survive the explosion, the ET/SRB-Shuttle separation would have to be at least a thousand feet or so. Even at this distance, any shock wave effects could still be dangerous. Now, even if all the above could be done in time and the Shuttle remain intact, could the Shuttle obtain an aerodynamic trajectory before hitting the ocean? I don't remember the altitude that the Shuttle was at when the explosion happened, but the Shuttle was on it's back and this is not a graceful way to start gliding. Also, correct me if I'm wrong, but I don't think that any sort of engines are available to help re-orient the orbiter during the abort (could the de-orbit engines be used?). Hence, only the control surfaces on the Shuttle could be used to establish a gliding (as opposed to plummeting) trajectory. To me, it seems doubtful that an abort could have succeeded in saving the lives of 7 astronauts or the orbiter. I am welcome to have any comments on my above reasoning, and I'd like to know if, in light of what I've said above, there was any reasonable chance for a safe abort. --Anthony Courtemanche ac%mit-oz@mit-mc