Article View: sci.space.shuttle
Article #3997Re: Throttling the Challenger
From: johng
Date: Thu, 29 Oct 1987 16:29
Date: Thu, 29 Oct 1987 16:29
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1798 bytes
In article <9298@tekecs.TEK.COM> philb@maya.UUCP (Phil Biehl) writes:
>In article <5270001@hpisof0.HP.COM> campbelr@hpisof0.HP.COM (Bob Campbell) writes:
>>SSME Specifications (Full power level)
>.
>.
>>Flowrates:
>> Total 1,130 lb/s 22,557 gpm
>> Hydrogen 160 lb/s 16,436 gpm
>> Oxygen 970 lb/s 6,121 gpm
>
>Does the above flowrates indicate tha actual combustion mixture present at the
>combustion chamber? If so then why is there a greater ratio than 2 parts H to
>one part O? I would think that the extra hydrogen would be unconsumed making
>the engine less efficient than it could be... What am I missing?
>
>Phil Biehl
True, some of the hydrogen goes unconsumed. There are two problems with
the perfect 8:1 mass ratio:
1) The metals of the engine cannot handle the temperature of the
reaction. So the hydrogen acts as a coolant.
2) *I'm not positive of this one* The temperature of the 8:1
reaction is enough to disassociate some of the water back into
hydrogen and oxygen therefore *lowering* the efficiency.
*Anybody know for sure?*
John Gregor
Technical Details
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<187@scdpyr.UUCP> <5270001@hpisof0.HP.COM> <9298@tekecs.TEK.COM>Show Full Headers
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Relay-Version: version B 2.10 5/3/83; site utzoo.UUCP Path: arc1-ca.pugleaf.net!utzoo!linus!philabs!prls!pyramid!decwrl!hplabs!hpda!uunet!mcvax!unido!ecrcvax!johng From: johng@ecrcvax.UUCP Newsgroups: sci.space.shuttle Subject: Re: Throttling the Challenger Message-ID: <447@ecrcvax.UUCP> Date: Thu, 29-Oct-87 11:29:45 EST Article-I.D.: ecrcvax.447 Posted: Thu Oct 29 11:29:45 1987 Date-Received: Sun, 1-Nov-87 20:36:05 EST References: <187@scdpyr.UUCP> <5270001@hpisof0.HP.COM> <9298@tekecs.TEK.COM> Reply-To: johng@ecrcvax.UUCP (John Gregor) Organization: ECRC, Munich 81, West Germany Lines: 29