Yep. If you have to move something big and move it fast, then Orion is good. Otherwise, there's no real point to it.SirNitram wrote:Quite. It's about the one situation where I'd advocate Orion.. Let's face it, it's been overhyped to hell.
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phongn, i dont know the maths, maybe you do. whats the speed of a 100kg probe accelerated by a force of 0.05 Newtons after travelling 20 million km say, and how long will it take to get there?
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Don't think I ever participated in any fighters-in-space thread.SirNitram wrote:That's what I've always heard, so I've been wondering if Koji went back for more of whatever he smoked during hte fighters-in-space and Singularity threads.
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That was my point about NERVA tho, the you can move some serious shit, and get it going to high speeds quickly. Putting a man on Mars? Thats a job for NERVA not ion rockets. Mining the asteroid belt? NERVA. Extracting He-3 from Uranus? NERVA or preferably fusion rockets.phongn wrote:Yep. If you have to move something big and move it fast, then Orion is good. Otherwise, there's no real point to it.
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I suggest you examine the G-forces involved in these short little burns. We don't want to laminate our astronaughts to the bottum of the ship.kojikun wrote:That was my point about NERVA tho, the you can move some serious shit, and get it going to high speeds quickly. Putting a man on Mars? Thats a job for NERVA not ion rockets. Mining the asteroid belt? NERVA. Extracting He-3 from Uranus? NERVA or preferably fusion rockets.phongn wrote:Yep. If you have to move something big and move it fast, then Orion is good. Otherwise, there's no real point to it.
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are there any conceivable limits to thrust produced by an ion drive? im finding that most ion drives put out mere tens of millinewtons.. they may have serious fuel use lengths, a good many times that of, say, NERVA, but theyre also producing much less thrust. MUCH less thrust..
im not sure, but i think a million newtons with an Isp of 1500 is better then 50 millinewtons with an Isp of 3000..
im not sure, but i think a million newtons with an Isp of 1500 is better then 50 millinewtons with an Isp of 3000..
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Again, you miss the point. Ion thrust is applied constantly. NERVA is a one shot that'll laminate your crew.kojikun wrote:are there any conceivable limits to thrust produced by an ion drive? im finding that most ion drives put out mere tens of millinewtons.. they may have serious fuel use lengths, a good many times that of, say, NERVA, but theyre also producing much less thrust. MUCH less thrust..
im not sure, but i think a million newtons with an Isp of 1500 is better then 50 millinewtons with an Isp of 3000..
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If you need to escape a gravity well, go ahead and use the nuclear drive. If you need to get somewhere fast, you can use a nuclear drive, but you're going to need enormous amounts of fuel, or you can use Orion (which still needs a good number of propellant).
For space probes you want efficiency, and that's where ion comes in.
For space probes you want efficiency, and that's where ion comes in.
Lowering the acceleration increases the time you can use the fuel you have, so its not an issue Nitram.SirNitram wrote:Again, you miss the point. Ion thrust is applied constantly. NERVA is a one shot that'll laminate your crew.
Can someone answer whether or not ion drives have a conceivable topoff to thrust..
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In that case, you don't even need the pusher plate. You just need a crater and even then you'll make your own perfectly sized crater by itself.phongn wrote:If you're moving rocks, you might as well install a pusher plate and put an Orion drive on it. It's useful for when you need high thrust and specific impulse.
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Well, you might get suface ablation and such - vaporizing precious material - so a pusher plate wouldn't be a bad idea.Gil Hamilton wrote:In that case, you don't even need the pusher plate. You just need a crater and even then you'll make your own perfectly sized crater by itself.phongn wrote:If you're moving rocks, you might as well install a pusher plate and put an Orion drive on it. It's useful for when you need high thrust and specific impulse.
If you're trying to do orbital bombardment or deflecting an asteroid, then it hardly matters
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Wikipedia is showing that ion drives top out around 10N of thrust (unknown isp) whereas NTRs are getting around 10000N of thrust with 900 seconds isp or so.kojikun wrote:are there any conceivable limits to thrust produced by an ion drive? im finding that most ion drives put out mere tens of millinewtons.. they may have serious fuel use lengths, a good many times that of, say, NERVA, but theyre also producing much less thrust. MUCH less thrust..
im not sure, but i think a million newtons with an Isp of 1500 is better then 50 millinewtons with an Isp of 3000..
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Well, vaporizing part of the asteroid is part of the idea initially, as it will increase the velocity of the asteroid and get where it is going faster, as it's not like a huge percentage of the asteroid's mass is being lost. Once it forms a nice crater that has been nice and baked, you'll have created a natural pusher plate on the asteroid's surface. Besides, the material lost can't possibly be more than the resources used to create a steel plate in the first place.phongn wrote:Well, you might get suface ablation and such - vaporizing precious material - so a pusher plate wouldn't be a bad idea.
If you're trying to do orbital bombardment or deflecting an asteroid, then it hardly matters
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But the plate, or at least a good chunk of it should be recoverable.Gil Hamilton wrote:Besides, the material lost can't possibly be more than the resources used to create a steel plate in the first place.
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To get rid of a 'roid coming at Earth it would be better to simply produce a reflective surface that nudges the rock away from a collision, most 'roids are collections of smaller rocks flying in tight formation. A nuclear blast could cause the formation to fragment and then you're in the shit with numerous, smaller missiles heading for Earth.
Proximity detonations are your friend.Admiral Valdemar wrote:To get rid of a 'roid coming at Earth it would be better to simply produce a reflective surface that nudges the rock away from a collision, most 'roids are collections of smaller rocks flying in tight formation. A nuclear blast could cause the formation to fragment and then you're in the shit with numerous, smaller missiles heading for Earth.
And none of those meganewton drives will see the light of day anytime soon. You still haven't brought forth a convincing argument as to why you should mount something as fuel-intensive as a NERVA-style drive on a probe headed to Jupiter.kojikun wrote:phong, there are some engines (or enginegroups?) that top out at 1.x million newtons. planned for use in interplanetary missions and stuff. but 10N ion thrusters is.. nothing
For manned missions, using high-thrust engines is desireable. But for probes? Not really.
Oh! I know why! Because it will be the first step to actually using the real thing in a practical interplanetary mission! :p
in al seriousness tho, youre right, it was foolish to say we should use an NTR for a probe. but who cares, it would look COOL
in al seriousness tho, youre right, it was foolish to say we should use an NTR for a probe. but who cares, it would look COOL
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Oh, it undoubtably would be reusable, but you'd need a ship of similar size to push the pusher plate and attach it to the asteroid. You don't need nearly as much resources to just make a natural pusher plate in the asteroid itself.Sea Skimmer wrote:But the plate, or at least a good chunk of it should be recoverable.
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The beauty of Orion is that you can do it on the cheap. No need to use ultra-lightweight/ultra-strong materials to build your vessel... you can easily make the sucker a mile long and constructed of concrete and rebar and it'll work just fine.
Massive project, though. Too much, in my opinion, for intrastellar missions. I could see it as a crude method of getting to nearby stars with less than a century of travel time (and easier to build than a solar sail).
Massive project, though. Too much, in my opinion, for intrastellar missions. I could see it as a crude method of getting to nearby stars with less than a century of travel time (and easier to build than a solar sail).
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