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Article #345

Re: Mars salt ?

#345
From: The Ghost In The Machine
Date: Sat, 28 Apr 2007 04:37
45 lines
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In sci.physics, Jeff Findley
<jeff.findley@ugs.nojunk.com>
 wrote
on Fri, 27 Apr 2007 13:26:32 -0400
<e56d3$46323246$927a2cda$25726@FUSE.NET>:
>
> "The Ghost In The Machine" <ewill@sirius.tg00suus7038.net> wrote in message 
> news:s1i9g4-1f8.ln1@sirius.tg00suus7038.net...
>> However, absent some major technological boost to our rocket exhaust
>> velocity (chemical rockets have poor performance but lots of thrust),
>> it's going to be expensive to get into space no matter what we do.
>
> I believe this is a flawed assertion.  The hard limit on launch costs is the 
> cost of fuel and oxidizer since that would be your only reoccurring cost for 
> a reusable launch vehicle.  And if you do the math, the cost of fuel and 
> oxidizer for a LOX/kerosene launch vehicle isn't bad at all.
>
> Jeff

It depends on the rocket performance -- v_e in Tsiolkovski's Rocket
Equation:

v_f = v_i + v_e * log(M_i/M_f)

Unfortunately, because Earth drags us all down, chemical rockets are
about the only things that have enough thrust to overcome their own
weight for sufficiently long to get into low Earth orbit and beyond.

Ion drives have nice high v_e but very low thrust, for example.

The best I can do is boil water a la Asimov using a nuclear
pile, and such rockets would have to be huge and very
high pressure.  You probably remember the Cassini mission
(which is now happily orbiting Saturn; AFAIK there's no
aliens out there complaining about the plutonium canisters
whose radioactive decay is used as a power source :-) ).
A nuclear reactor would generate even more heat -- and
not for the purpose of producing lifting thrust.

-- 
#191, ewill3@earthlink.net
"Woman?  What woman?"

-- 
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From: The Ghost In The Machine <ewill@sirius.tg00suus7038.net>
Subject: Re: Mars salt ?
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