Path: utzoo!attcan!utgpu!jarvis.csri.toronto.edu!mailrus!wuarchive!brutus.cs.uiuc.edu!ginosko!uunet!zephyr.ens.tek.com!tekig5!robina From: robina@tekig5.PEN.TEK.COM (Robin Adams) Newsgroups: sci.space.shuttle Subject: Re: Why 3 SSME's? Message-ID: <4900@tekig5.PEN.TEK.COM> Date: 11 Oct 89 18:22:20 GMT References: <538.252A3A3B@mamab.FIDONET.ORG> Organization: Tektronix Inc., Beaverton, Or. Lines: 32 In article <538.252A3A3B@mamab.FIDONET.ORG>, Mike.Pompura@f49.n363.z1.FIDONET.ORG (Mike Pompura) writes: > I submitted a proposal to NASA and Rockwell that involved the escape > sequence for a shuttle PES system. > > Basically what it was is a method of escape for the astronauts in the > event of a Challenger-type mishap. It was dismissed as not being cost > effective. > > I suggested that the pressurized inner crew cabin be severed from any > remaining orbiter pieces by explosive bolts multitude of explosives already>, and provided with a series of drogue > and main parachutes stowed near the front landing gear, attached to the > inner crew cabin. In the event of ............. -- I agree. I've always felt NASA's first obligation is to ensure that all aspects of Challenger should not be able to repeat. I would however go a couple of steps further on your proposal and suggest: 1. The addition of a small escape rocket to get them out of the immediate area. 2. Quick electrical (and other) disconnects between the inner cabin and orbiter to facilitate seperation. * |_____ * | |/ Robin * | Adams |_____|\ * |