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|    Message 44,927 of 45,986    |
|    alien8752@gmail.com to All    |
|    Re: Antimatter Nuclear Pulse    |
|    06 Apr 17 11:10:02    |
      From: nuny@bid.nes              On Tuesday, April 4, 2017 at 7:18:50 AM UTC-7, 0something0 wrote:       > I thought that a pure antimatter-powered nuclear-pulse was a interesting idea               A quick Google doesn't inspire me with its practicality.              > that deserved a thread all of its own. So, here is a question that begs to be       > asked:        >        > How do we calculate the thrust and the Isp of an antimatter-powered nuclear       > pulse?               The general idea is to mix small amounts of antihydrogen with a larger mass       of ordinary hydrogen. The implementations so far suggested (per the Wiki and       other sources) don't seem to me to be particularly efficient.               You either load a kilogram or so blob of cold hydrogen plus a microgram of       antihydrogen in a sacrificial Penning trap and allow them to mix Orion-style       then get thrust against a non-sacrificial magnetic field that makes up the       "exhaust bell", or inject        pellets of antihydrogen into a continuous stream of hydrogen producing       individual bangs of variable yield depending on how wide open the hydrogen       throttle happens to be at the moment, again getting thrust by reaction against       the engine's magnetic field.               In the first case, as Luke Campbell points out, much of the reaction       products don't actually provide thrust (because they ignore the engine's       magnetic "bell"), and some are actively hazardous to the engine structure and       presumed crew (do it just right        and it's a neutron bomb). You get individual pulses of thrust just like the       original Orion. How much? Total released energy minus the unusable part that       ignores the magnetic bell. It seems to me that it gets very handwavy depending       on how quickly the        reactions proceed vs. confinement time in the bell. The engine dimensions will       be critical.               In the second case, the continuous hydrogen stream can contain some of the       non-thrust products (decaing neutral pions)leading to more heating and       presumably more thrust, but does the stream stay hot enough to keep fusing       between pellets? If so there        will be a constant thrust component with the pulses superimposed on top of       them. You could get variable thrust by opening the hydrogen throttle and       injecting the pellets more often while keeping the constant thrust-pulse       thrust ratio constant.               I *think* the continuous stream approach will be more efficient but that       also depends on confinement time vs. reaction rate, but only if the engine is       big enough to allow the stream to capture and utilize the "wasted" products       before they escape.               Deducing Isp is beyond me. I'll have to think about it a lot more.                      Mark L. Fergerson              --- SoupGate-Win32 v1.05        * Origin: you cannot sedate... all the things you hate (1:229/2)    |
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