A Fusion Thruster For Space Travel
spectrum.ieee.org
spectrum.ieee.org
"The specific power of the proton-triggered boron fuel would be so great that a mere mole of it (11 grams) would yield roughly 300 megawatts of power. (According to Chapman, using this aneutronic fusion technique with helium-3 isotopes would yield 493 MW per mole. But boron is a more attractive fuel source because it is abundant on Earth and helium-3 is scarce.)"
This looks like nonsense. I think it was supposed to be megawatt-hour -- the quote is essentially correct, after you r/megawatt/megawatt-hour/, r/MW/MWh/, and r/specific power/specific energy/.
No idea why they are using this unit outside its native context (electricity generation).
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I don't know about specific power, but the (theoretical) specific impulse is very good. The exhaust speed of the fusion alphas is sqrt(2 * 2.9 MeV / 3.7 GeV/c^2) = 1.2e7 m/s (or 0.04 c). Since these alphas constitute all the mass of the fuel/propellant (which are the same in this scheme), this is also the effective exhaust velocity. Or a specific impulse of 1.2e8 seconds.
This is one of the best specific impulses conceived of, and (I think) is about the theoretical limit for a fusion-powered rocket carrying its own reaction mass.
http://en.wikipedia.org/wiki/Spacecraft_propulsion#Table_of_...
For some reason I don't see it represented on this (very big) wiki page. They do have the "fission fragment rocket", which is conceptually the same thing applied to fission reaction products.
I was wondering if maybe they meant J rather than W, but you must be right -- 300MJ/mol doesn't sound like much.
http://www.nndc.bnl.gov/chart/reCenter.jsp?z=2&n=2
http://www.google.com/#sclient=psy&hl=en&authuser=0&...
edit: Another source for "8.68 MeV", which doesn't require math:
http://en.wikipedia.org/wiki/Nuclear_fusion#Criteria_and_can...
The article doesn't say that directly, I'm inferring it from the fact that if it was net-energy positive, this would not be "hey, this might make more efficient propulsion", but "HEY EVERYBODY, HOLY COW, FUSION IS HERE!". I am comfortably with this inference.
I also would imagine the efficiency in question is that it has a very high specific impulse [2], and thus requires very little mass, not anything else. Satellites in the inner solar system generally don't have a power problem, they metaphorically just stick a cup out the window and grab some of the power just streaming by them nearly continuously. They have a mass problem. Converting solar power mass-efficiently to thrust is a big win.
For a power plant they'd need a laser that doesn't exist yet, but it looks like commercially-available lasers could do the experiment.
http://en.wikipedia.org/wiki/Polywell#Possibility_of_net_pow...
Anyone else think this sounds like sci-fi technobabble?