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: SRB Telemetry Clues Message-ID: <8602011714.AA03500@s1-b.arpa> Date: Sat, 1-Feb-86 11:17:21 EST Article-I.D.: s1-b.8602011714.AA03500 Posted: Sat Feb 1 11:17:21 1986 Date-Received: Mon, 3-Feb-86 06:23:47 EST Sender: daemon@ucbvax.BERKELEY.EDU Organization: The ARPA Internet Lines: 30 The NY Times today (2/1/86) reports that telemetry indicates the right (far) SRB experienced a 4% drop in thrust and a 30 lb/in^2 drop in pressure starting 10 seconds before the explosion. The main engines and SRB nozzles were swivled at that time to try to compensate. Also, telemetry indicates the main engines stopped several seconds before the explosion, apparently because the oxygen line running down the side of the ET was cut. My guess of the course of the accident is this: (1) the right SRB was faulty, (2) when the burn-though on the side of the SRB occured (either because of cracked propellant or casing) a jet of hot gas hit the ET near the oxygen line, (3) it took several seconds for the insulation and metal to burn through, (4) when the oxygen line went gas began escaping and perhaps the tank structure itself (aluminum) burned in the hot oxygen gas, (5) just before the explosion the flames may have set off the range-safety charges on the ET, allowing the fuels to mix and explode. This could explain the small explosion that occured several frames before the big blast. It looks like proper software could have saved the shuttle. The proper course would have been to jettison the SRB's as soon as one acted up. Unfortunately, SRB's have varying thrust, so perhaps NASA didn't want to jettison one for just a 4% variation. Even so, the shuttle could have tried to get away when all the main engines failed, although it's not clear enough time remained for it to get clear. Does anyone know if the shuttle was in a position to return to Kennedy, or did it already have too much lateral velocity to glide back on its own? Also, how close is the oxygen line to the right SRB? If it runs down the right side of the ET this could be considered a serious design error (similarly for the range safety charges).