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Wed, 10 Apr 91 01:51:50 -0400 (EDT)
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Date: Wed, 10 Apr 91 01:51:45 -0400 (EDT)
Subject: SPACE Digest V13 #385
SPACE Digest Volume 13 : Issue 385
Today's Topics:
Re: Laser launchers
Re: SPACE Digest V13 #364
Re: comsat cancellations and lawsuits
Re: comsat cancellations and lawsuits
Voyager CD-ROMs On-Line
Re: Launch Technology:
Re: comsat cancellations and lawsuits
SPACE Digest V13 #377
Re: Space technology
Administrivia:
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/_ /| /____/ \ /_ /| Ron Baalke | baalke@kelvin.jpl.nasa.gov
| | | | __ \ /| | | | Jet Propulsion Lab |
___| | | | |__) |/ | | |__ M/S 301-355 | Change is constant.
/___| | | | ___/ | |/__ /| Pasadena, CA 91109 |
|_____|/ |_|/ |_____|/ |
------------------------------
Date: 9 Apr 91 14:47:58 GMT
From: sun-barr!olivea!samsung!zaphod.mps.ohio-state.edu!caen!news.cs.indiana.edu!maytag!watmath!watdragon!watyew!jdnicoll@apple.com (James Davis Nicoll)
Subject: Re: Launch Technology:
In article <HESKETT.91Apr7144310@polymnia.titan.tsd.arlut.utexas.edu> heskett@titan.tsd.arlut.utexas.edu (Donald Heskett) writes:
>The book "Ignition!" (written in the '60s, I think) mentioned that the
>highest specific impulse that had been achieved at that time was 542
>seconds. This was achieved with near-satanic propellant combination of
>lithium, fluorine and hydrogen. Does anyone know if any further work
>was ever done with this propellant combination?
>
>Needless to say, 1) it's probably not a good idea to operate
>fluorine-fueled propulsion systems in proximity to population areas or
>the ozone layer and 2) it's not a good idea to carry this stuff in
>the Shuttle's payload bay. The combination would only seem to make
>sense in the upper stage of an expendable launcher.
What's the cost per tonne of lithium, fluorine and hydrogen,
what's the cost of storing and using them and how do those two costs
compare to the costs associated with standard fuels? A wild guess might
that the higher Isp is nice, but that the problems of handling fluorine