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#11
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Mission to Alpha Centauri
Iain Why do you need staging in space?
Jim The same reason you would need staging anywhere; it's a method of Jim achieving the necessary mass ratio. Maybe I was being unclear. Yes, staging helps you get a larger mass ratio. But in general, how do you get a large mass ratio? - small engine mass relative to payload. - small tank mass relative to payload. - large propellant mass relative to payload. If you are willing to have very low acceleration, then your engine mass can be small (don't need so much thrust) and tank mass can be small (don't have to support so much weight for a given amount of mass). At 10 G acceleration, a single stage mass ratio of 5 requires some pretty good engineering. At 1 G acceleration, the same materials, etc should get you a mass ratio of 50 in a single stage. At .01 G acceleration, think about mass ratios of 5000. Of course, at mass ratios of 5000, you have to start thinking about other problems. Your engine burn will last a very long time, and so your tanks and engines have to deal with reliability problems ordinary rockets simply ignore. My point was that if your trip is going to take months or years anyway, you can afford to wait through engine burns of days or months, and very low accelerations are perfectly reasonable, and so very large single-stage mass ratios are possible. So why bother with staging? Is that more clear? |
#12
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Mission to Alpha Centauri
In article ,
Roger Stokes wrote: Very low acceleration would prolong trip time so I assumed a certain minimum acceleration of (say) 0.1g would be needed to actually be going at 0.2c for most of the trip. A useful rule of thumb is that 1G is roughly c/year. So at 0.1G, you need about two years to accelerate to 0.2c. Somewhat lower acceleration would be acceptable, but it can't be a lot lower or the acceleration time starts to dominate the trip time. At 0.01G, you are halfway to Alpha Centauri at engine cutoff. That is grossly wasteful at interstellar speeds, because it means that your average speed is rather less than your final speed. It takes about 30 years to reach Alpha Centauri that way, but it only takes about 45 if you stop accelerating when you reach 0.1c. Doubling the delta-V is an awfully expensive thing to do when it only reduces the trip time by 1/3. Another useful rule of thumb: acceleration distance should be no more than 10% of the total trip distance. For Alpha Centauri and a cruising speed of 0.2c, that means you need about 0.05G minimum. What values of space fuel tank mass/volume ratio are achievable today - depends on acceleration, and type and volume of fuel I know but any figures? Also depends *tremendously* on what's in them, what pressure they're at, and on whether there are any aerodynamic constraints. With minimal pressure, low acceleration, and no aerodynamics, it should be feasible to make tank mass very low... *provided* the tank walls don't have to include thermal insulation too. Which might be feasible out in interstellar space, if you are very careful to shield the tanks from engine heat and payload warmth. The Daedalus first-stage tanks were 60m-dia titanium-alloy spheres weighing about 25t each empty. -- MOST launched 1015 EDT 30 June, separated 1046, | Henry Spencer first ground-station pass 1651, all nominal! | |
#13
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Mission to Alpha Centauri
"Elmar Moelzer" wrote:
Hey Henry! Thanks for the explanation! I do not really understand that smoke- cloud- thing in full detail. I suppose they would be using some sorts of rockets to spread the gas- cloud ahead of the mothership (when simply blowing it out in front of the mothership the gascloud would continually drifft away further and further)? Wouldnt hitting that smokecloud be dangerous too? I mean that this way one would replace a potentially existing dangerous object with a certainly existing dangerous object, right? You're not thinking right. You've gotta think *relative* velocities. So you spew a smoke or gas cloud out, what's the relative velocity going to be? Low, a few km/s at most if it's rocket exhaust going the wrong way. That's nothing to sneeze at but it's easy to design a ship to withstand the effects. But what's the relative velocity going to be between the gas / dust and junk in space? Yup, 0.2 c, 60 *thousand* km/s. 44 *million* times as much relative kinetic energy per kg as with rocket exhaust from even a high-performance nuclear thermal rocket, 4 times that in relation to rocket exhaust from an ordinary chemical rocket. That makes all the difference. The relative kinetic energy per kg is sufficient to melt, vaporize, and even ionize any material on impact. The trick is throwing up enough mass in between your ship and incoming debris to guarantee incoming objects interact with enough mass to release enough energy to do that, but that's an easy problem given the rarity of large objects even in interplanetary space. Running into a several km asteroid would be a problem, but for ordinary debris (dust, pebbles maybe) that you are most likely to run into, the gas / dust shield would vaporize it quite effectively. So, the relativistic effects do not increase in a linear way? How strong would the effect be at 0.4 light then (just so I can calculate this)? Completely non-linear. It kinda has to be to go to infinity at c. What you need is "gamma", which is the relativistic scaling factor, it's sqrt(1-(v/c)^2). As you'll notice, it is 1 at v=0 and 0 at v=c. "Relativistic mass" increases as 1/gamma (m0/gamma), as does time-dilation. Length contraction decreases directly with gamma. You'll notice that 1-gamma is a mere 0.02 at 0.2 c, in other words, at 0.2 c "relativistic effects" only manifest as a difference of around 2%. And 1-gamma doesn't get up to 0.5 (i.e. relativistic effects of around 2x) until 0.87 c. |
#14
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Mission to Alpha Centauri
In article lekom.at,
Elmar Moelzer wrote: I do not really understand that smoke- cloud- thing in full detail. I suppose they would be using some sorts of rockets to spread the gas- cloud ahead of the mothership (when simply blowing it out in front of the mothership the gascloud would continually drifft away further and further)? Yep, the mother ship would have little auxiliary vehicles to spread it. The sub-probes probably would just have to blow it ahead, reducing its effectiveness. Wouldnt hitting that smokecloud be dangerous too? I mean that this way one would replace a potentially existing dangerous object with a certainly existing dangerous object, right? Anything that's in the path of an object moving at 0.2c is toast. :-) The only question is whether the 0.2c object is toast too. The assumption is that the preservation of minor meteorites is not a priority for the probe. So, the relativistic effects do not increase in a linear way? How strong would the effect be at 0.4 light then (just so I can calculate this)? Correct, they are strongly nonlinear. The formulas can get messy, but a lot of the effects scale with 1/sqrt(1 - v^2/c^2), which is easy enough. -- MOST launched 1015 EDT 30 June, separated 1046, | Henry Spencer first ground-station pass 1651, all nominal! | |
#15
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Mission to Alpha Centauri
"Elmar Moelzer" wrote in...
Hey Henry! Thanks for the explanation! [...] So, the relativistic effects do not increase in a linear way? How strong would the effect be at 0.4 light then (just so I can calculate this)? Is this one of those 1/(1-beta) things? Dang, why does that seem so long ago....someone musta shifted my quantum clock by 30 years. /dps |
#16
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Mission to Alpha Centauri
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#17
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Mission to Alpha Centauri
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#18
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Mission to Alpha Centauri
Laser light sails are capable of sending payloads to stars.
Sunlight is intercepted by a large thin film concentrator. This illuminates a solar pumped laser. The laser energy is directed through a beam forming device. The beam is reflected by a thin film mirror which causes momentum to be transferred to the mirror. A payload is attached to the mirror which is carried to high speeds along with the mirror. No fuel is used aboard the craft during interstellar transit. Bob Forward and others have proposed two-stage mirrors that separate at the target star into a donut shaped annulus and a donut-hole shaped central disk. The annulus is shaped to focus light on the smaller disk as they separate. The smaller disk now carries the payload. Momentum is transferred to both the larger annulus and the smaller disk simultaneously. The large annulus continues to accelerate. The small central disk is slowed. Ultimately, the payload enters the target star system. The payload can be equipped with microfission based nuclear pulse rocket which gives it the legs to zip throughout the target star, collecting data and beaming it back to Earth. More advanced systems can be contemplated. Larger systems can carry people and industrial cargo. Such systems, developed for interplanetary settlement, can be adapted for use around target star systems possessing suitable planets and planetoids. Imagine that star colonies are established around nearby planetary systems, complete with their own industrial infrastructure. Each is equipped with their own laser light sail set up to send payloads to neighbors around them. In this way, payloads can be sent back to Earth from the colonies, incoming payloads can be slowed down using local laser light energy thus reducing the cost and increasing the payload, and payloads can be forwarded to destinations further outward. In this way, an expanding network of laser beam spaceways can be constructed giving humanity access to the billion or so stars contained in the Perseus Nebula surrounding the Sun in our arm of the Milky Way galaxy. Imagine now, that a collection of nearby star colonies coordinate their affairs through radio telescope and arrange to collide large shaped iron masses at considerable speeds at a mutually agreed upon location. Black holes created in this way can themselves interact to create all sorts of weird effects. Among them, is the creating of new black holes from the decay of the vacuum due to the powerful gravity effects of the black holes you built up from iron. In this way, huge collections of black holes - black hole dusts - can be created. Such dusts can interact via all the forces of nature, as well as temporal loops. This opens up a whole new era of physics and engineering, leading to among other things, a sort of superluminal travel involving time machines. Once we have time machines and gravity drives based on the decay of synthetic black holes we will have the ability to traverse the visible cosmos in very short times scales (hours) and return home about the time we left. If in our journeys we discover naturally occuring time violating regions, we will then have the potential of travelling back in time before the epoch described above - essentially giving intelligence access to all of space and time - from the very beginning of the cosmos to the very end. At this point we can say travel through space and time has achieved all its major goals. Unconstrained by technical limits, we are then constrained by our imagination only. * * * LASER LIGHT SAIL REFERENCES * * * Introduction to Laser Light Sail concept; http://ffden-2.phys.uaf.edu/213.web....ightsails.html Actual experiment with laser light sail; http://www.space.com/news/lasersail_000301.html More laser light sail stuff; http://www.itsf.org/brochure/solarsail.html http://www.sciam.com/article.cfm?col...A8809EC588EEDF http://solarsail.jpl.nasa.gov/introd...ails-work.html http://www.portal.telegraph.co.uk/connected/main.jhtml;$sessionid$D5TRTHIAABN4TQFIQMGSFF4AVCBQ WIV0?view=DETAILS&grid=P8&targetRule=10&xml=%2Fcon nected%2F2002%2F02%2F19%2Fecnaa519.xml http://www.sff.net/people/Geoffrey.L...ghtsail89.html http://www.niac.usra.edu/files/studi...df/4Landis.pdf * * * SUN PUMPED LASER REFERENCES * * * http://hep.uchicago.edu/solar/laser.html http://www.nap.edu/books/0309045770/html/97.html http://www-mpl.sri.com/projects/ted5985-1.html * * * MICRO-FISSION REFERENCES * * * http://www.engr.psu.edu/antimatter/Papers/ICAN.pdf http://www.spacetransportation.com/a.../1A_Smith.html http://highwaytospace.com/ast/presen...s/1a_smith.pdf * * * SYNTHETIC and COLLIDING BLACK HOLE REFERENCES * * * http://abcnews.go.com/sections/tech/...y.current.html http://www.sciencenews.org/20020803/fob4.asp |
#20
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Mission to Alpha Centauri
In interstellar space, minimal. It does need a shield on the front
against gas and fine dust, and some attention to cooling of the shield. Hitting even a pebble would be deadly, but such objects are extremely scarce out there. Unfortunatly that's a long "slow wake zone" till you reach debris-free interstellar space. |
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