Return-Path: Received: from [65.33.165.125] (account marv@lancaironline.net) by logan.com (CommuniGate Pro WebUser 4.2.5) with HTTP id 554760 for lml@lancaironline.net; Fri, 03 Dec 2004 10:01:29 -0500 From: "Marvin Kaye" Subject: Re: [LML] Cabin Pressurization in SpaceShipOne To: lml X-Mailer: CommuniGate Pro WebUser Interface v.4.2.5 Date: Fri, 03 Dec 2004 10:01:29 -0500 Message-ID: In-Reply-To: <002001c4d945$88f2a270$0200a8c0@CYBERMAX> References: <002001c4d945$88f2a270$0200a8c0@CYBERMAX> X-Priority: 3 MIME-Version: 1.0 Content-Type: text/plain; charset="ISO-8859-1"; format="flowed" Content-Transfer-Encoding: 8bit Posted for "Larry Henney" : Jeff, It's not the whole answer but the Nov Sport Aviation article on page 38 acknowledges that White Knight bleed air is ducted into SS1 for purposes such as keeping the nitrous oxide at 66F, engine bay, and mechanisms. The unstated inference might be that pressurization also comes from this bleed air. This and another related statement on page 37 "every aspect of the pressure system is digitally monitored, and any leak of any kind is instantly reported on the TONU" leads me to believe that they are totally sealed and only face a differential change in pressure after release from 50K. I'm sure some math genius could tell us how much atmosphere is left above 50K. Perhaps SS1 is pressurized to let's say 5000' MSL upon release. The question remains, to what altitude would the cabin climb when the outside pressure drops from 50K up to zero (space?). And would my ears pop? Inquiring minds need to know. Larry """ So, what is the cabin pressure differential inside SpaceShipOne? And how does it get this...bleed air of the engines...doubtful? And how does it control it, so you don't get the full magilla at 50,000' and overpressurize your brains during the initial stage? """