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is near light speed achievable? |
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| Jan10-11, 08:47 AM | #18 |
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is near light speed achievable? |
| Jan10-11, 08:53 AM | #19 |
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I know where you're coming from; I can smell the crackdom too. It's just that my philosophy is to facilitate much as possible (peppered with caveats and warnings) until they violate physics. I don't see the good in shutting people down on principle. Anyway, that's two takes on the same question. Good for the OP to see differing viewpoints. |
| Jan10-11, 05:26 PM | #20 |
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Mentor
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| Jan10-11, 09:28 PM | #21 |
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Still, IMO, these kinds need our help more than others. |
| Jan11-11, 09:24 AM | #22 |
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here is the link https://sites.google.com/site/exhaus...earpropulsion/
be specific on why it will not work I am already half convinced it wont work |
| Jan11-11, 09:33 AM | #23 |
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You are ignoring conservation of momentum.
It doesn't matter how slowly you stop the ball, it imparts an equal reaction force towards the rear as it initially did towards the front. They cancel out. As per my email, all of the kinetic energy of the ball is converted to heat whether you stop it instantaneously on the back wall of the space craft or through your "friction tube". This is independent of momentum. You can't convert the momentum to heat. The problem with your understanding is that you believe only a quantity of the kinetic energy becomes heat and the rest goes towards a counter-acting force. Thus, the reaction acting against the forward motion is less than the initial forward acting motion, giving a net forward motion. This is incorrect and a flawed understanding of the physics of the system. You have combined two different concepts and drawn an incorrect conclusion. I recommend reading up on Conservation of Momentum and Conservation of Energy. |
| Jan11-11, 10:46 AM | #24 |
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Yes, energy is lost due to friction. But it is not lost from the kinetic enrgy of the craft, it is lost from the device that pushes the ball forward (whatever device or mechanism that might be, it doesn't matter). That mechanism will have to work harder against friction. i.e. it will have to put out more energy (energy lost to heat friction) while the ball will simply move the same amount. So, ultimately, your device uses a mechanism that works hard to create friction which creates waste heat. None of that has anything to do with the device moving. In principle: there is absolutely nothing you can do inside the craft to move the craft's centre of mass. |
| Jan11-11, 08:08 PM | #25 |
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| Jan11-11, 08:13 PM | #26 |
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"I propose X as viable. Here's a link." "Your link is not convincing." "You do your own homework." |
| Jan11-11, 08:20 PM | #27 |
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This image here shows it requires a lens "30,000 miles across" and "100 billion light sensitive processors". I also refer you to his own paper, equation 35, page 4 where he shows the lens required for a 1km sail is 50,000km with an estimated mass of 50,000 tons. Along with said system requiring "excessively large" amounts of power. Paper available here: http://www.boomslanger.com/images/starwisp.pdf Your exact words were: "This idea seems to me to be the most viable means for us to send probes to the nearest stars.". Based on the above, I'd say that is not so. I'm not exactly sure what I did to deserve that reaction, but I'm pretty sure the rules are that you back up your claims. |
| Jan11-11, 09:30 PM | #28 |
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Here's the technical paper: http://www.boomslanger.com/images/starwisp.pdf I wasn't making a claim other than my opinion of comparative viability. The starwisp doesn't need invented technology such as cracking fusion, only some reasonable engineering and hardware design. We could begin tomorrow if we had the will. The infrastructure could be recycled to home power production from orbit and pay for itself over time. (That may be a stretch but if not the infrastructure could power space based industry and knowledge ALWAYS pays eventually) We could start smaller using wisps to explore e.g. the Oort cloud and probe past the heliopause. Oh, and when the alien invaders come calling we can roast them in their ships with our microwave weapons battery!
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| Jan11-11, 09:37 PM | #29 |
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Getting 50,000 tons into space and then the construction of said materials for a 50,000km emitter lens is considered "reasonable engineering"?
What was the cost per kg to get stuff into space? |
| Jan11-11, 09:58 PM | #30 |
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BTW the fresnel lens is not the only option. One can phase correlate the array of transmitters. (I think... I'll have to do some calculations....but not tonight, classes start tomorrow, delayed by the ice storm and I've got to teach at 8:00am.) Of course one is talking about a vast engineering project, far grander than anything we've ever done before. But it is feasible within current technology and reasonable extrapolation of engineering. |
| Jan11-11, 10:03 PM | #31 |
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I may not like it, but it's certainly possible for getting a 1km array up to near relativistic speeds. |
| Jan11-11, 10:07 PM | #32 |
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But I challenge you to suggest a cheaper way to get a probe to the nearest star. Again I said "most" viable, not "super-easy-cheap-why-didn't-Columbus-just-bypass-America-and-go-to-Alpha-Proxima" viable. |
| Jan12-11, 05:58 AM | #33 |
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Here's some math for the curious...
Figure the sustained acceleration you need to reach a given % of c (including over 100%) in simple Newtonian physics then take the hyperbolic tangent. That's the relativistic % of c. Example you boost to what would be c in Newton's universe, that's about 8500 g-hours (almost a year accelerating at 1 g) and you will get to tanh(1)= (about) 0.76 or 76% c as seen by the people watching from your starting frame. To figure the energy you need, you would take the hyperbolic cosine minus 1 times the mass (the minus 1 subtracts out the initial mass-energy). E.g. cosh(1) = 1.543 so you need about 54% of the payload mass times c^2 in energy to get up to 76% lightspeed. That's about 48,900 TeraJoules per kg or 48,900 Tera-watt seconds per kg payload... or 13.6 TW hours per kg or about 19 GW months. Figure the output of a few industrial scale power plants sustained over a month to accelerate at 10 or 12 gees per kg payload. That's delivered to the payload. With a beamed source (light or microwaves or whatever) one must figure one or two factors of 10 for losses and beam spreading. It's not unthinkable but certainly would require we keep the payload size under say 20kilograms and a major industrial presence in space. And .76c may be too ambitious, more like .01c or .005c. Something we could imagine happening in the year 2200. I mentioned we wouldn't need to assume new tech (like cracking fusion) but we'd probably need orbital fusion power plants to get that kind of power output or some other energy production improvement. |
| Jan12-11, 06:50 AM | #34 |
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