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- Newsgroups: sci.space
- Path: sparky!uunet!usc!cs.utexas.edu!torn!watserv1!watdragon.uwaterloo.ca!watyew!jdnicoll
- From: jdnicoll@watyew.uwaterloo.ca (James Davis Nicoll)
- Subject: Re: Antimatter (was propulsion questions)
- Message-ID: <Bs0rs0.LGJ@watdragon.uwaterloo.ca>
- Sender: news@watdragon.uwaterloo.ca (USENET News System)
- Organization: University of Waterloo
- References: <711790218snx@osea.demon.co.uk> <LNweoB1w164w@sys6626.bison.mb.ca> <BrwF7B.FMJ@watdragon.waterloo.edu> <mikew.712022819@kpc.com>
- Date: Sun, 26 Jul 1992 23:26:23 GMT
- Lines: 28
-
- In article <mikew.712022819@kpc.com> mikew@kpc.com writes:
- >jdnicoll@watyew.uwaterloo.ca (James Davis Nicoll) writes:
- >> Given that one can mix the antimatter-reaction mass ratio to get
- >>the Vexhaust one wants, the dangers of standing in the vicinity of the
- >>exhaust of an antimatter powered ship could be *identical* to that of
- >>standing inthe vicinity of a conventional ship.
-
- >Actually there is one piece of information missing here. In a conventional
- >rocket most of the exhaust is being used to push more fuel closer to orbit.
- >In an antimatter rocket, you have a much higher payload/fuel ratio, so for
- >the same payload, there will be much less exhaust.
-
- Odds are the antimatter will be the expensive component of the
- reaction-mass/'fuel' mix, and so the am-reaction-mass ratio will be such
- that the am is used as efficiently as possible. The mass ratio is smallest
- if there is a 50% am, 50% matter mix, but that uses much more am then
- a mixture of am/m which is mostly matter. I would bet the population of
- Gary, Indiana that if antimatter energised propulsion systems are used
- from Earth's surface to reach orbit, the exhaust velocity will be in the
- 10 km/s range, rather than close to C.
-
- Also, 'pure' photon drives tend to produce oodles of nasty
- hard radiation which could very well fall outside the allowable ranges
- of todday's litigation prone society, plus they suck up power like a
- mad fiend.
-
- James Nicoll
-
-