| Subject: Re: NASA blunts opposition to nuclear rocket//NASA=Never A Straight Answer |
| From: "Paul M. Koloc" <pmk@plasmak.com> |
| Date: 25/12/2003, 08:07 |
| To: LawsonE <nospam@nospam.com> |
| Newsgroups: alt.alien.visitors,alt.alien.research,alt.paranet.ufo,alt.paranet.abduct,sci.skeptic,sci.astro |
LawsonE wrote:
"Paul M. Koloc" <pmk@plasmak.com> wrote in message
news:3FE76759.2040909@plasmak.com...
The Carnot efficiency is based on the throughput temperature of the
thermal source. The higher the temperature, the better the efficiency.
As long as the system doesn't melt, of course...
Excellent point. The system is pulsed (cycled like a diesel). The
compression (burn) chamber walls are protected by the presence of the
fusion radiation absorbing compression fluid for each new pulse.
Additional protection can be applied by injecting onto the walls of a
fluid of the appropriate volatility to produce any needed additional
cooling by sublimation. Since the pule burn will be fast, the thermal
diffusion loss from the compression blanket to the compression wall is
minimized. The further adiabatic expansion of the fusion heated
compression blanket as it is released into the inductive MHD generator
will also help to cool the system as well as produce efficient electric
power to drive both the thrust engine and the compression burner.
--
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