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Article #8906Re: Solid State Fusion for Launchers
From: Henry Spencer
Date: Sat, 01 Apr 1989 22:49
Date: Sat, 01 Apr 1989 22:49
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In article <1989Mar31.163051.5961@cs.rochester.edu> dietz@cs.rochester.edu (Paul Dietz) writes: >The second possibility is to use a smaller fusion reactor to preheat >fuel and/or oxidizer before injection into a conventional chemical >engine. This would increase the Isp beyond that possible with >chemical fuels alone. I doubt the practicality of this. Existing oxyhydrogen rockets already run fuel-rich partly to *cool* the exhaust a bit (and thus reduce thermal dissociation of water into oxygen and hydrogen). It might help the less energetic fuels like hydrazine, but why bother? If the power densities stay low, the big use will probably be as a power source for electrical propulsion in space. -- Welcome to Mars! Your | Henry Spencer at U of Toronto Zoology passport and visa, comrade? | uunet!attcan!utzoo!henry henry@zoo.toronto.edu
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Newsgroups: sci.space Path: arc1-ca.pugleaf.net!utzoo!henry From: henry@utzoo.uucp (Henry Spencer) Subject: Re: Solid State Fusion for Launchers Message-ID: <1989Apr1.224916.22484@utzoo.uucp> Organization: U of Toronto Zoology References: <1989Mar31.163051.5961@cs.rochester.edu> Date: Sat, 1 Apr 89 22:49:16 GMT