Red mercury theatre: http://www.tor.com/stories/2012/07/a-tall-tail On Thu, Feb 19, 2015 at 4:27 AM, Monroe L. King Jr. < monroe@xxxxxxxxxxxxxxxxxx> wrote: > If compression of that level where possible I can think of a gillion > better ways than compressing air for propulsion. > > Illogical > > Monroe > > > -------- Original Message -------- > > Subject: [AR] Re: Way OT question: degerate matter thrusters? > > From: Peter Fairbrother <zenadsl6186@xxxxxxxxx> > > Date: Thu, February 19, 2015 1:46 am > > To: arocket@xxxxxxxxxxxxx > > > > > > On 18/02/15 21:22, Lloyd Droppers wrote: > > > I'm not a physicist so I won't talk much about the properties of > > > degenerate matter. Rather, I will stay with the cold, hard science of > > > single stage to orbit cold gas thrusters made of space elevator fiber. > > > > > > The basics of this are the rocket equation > DV=Isp*ln(m_initial/m_final). > > > You said orbit, so lets say LEO DV=9200 m/s. And if we just use N2 > > > instead of air (it's 75% of air, and you probably don't want Oxygen at > > > that high of a pressure) and assume a simple rocket at 300K Chamber > > > temperature (I don't know how to design a degenerate Air to room > > > temperature heat exchanger, but I'll assume it is possible) and a gamma > > > of 1.4 gives a 1.7 max CF from RPE so that gives you a 75s Isp. This > > > means that your initial mass would have to be 270000x larger than your > > > initial mass so that is a tiny payload, but it is physically possible. > > > > > > If you just need to get to space before your other engines can kick in, > > > that is 1500 m/s DV. This is only a 7.7x initial mass to final mass > > > ratio - about the same mass ratio as a single stage rocket is today. > > > > > > Now, let's run some numbers for real world best case Air rockets. > First, > > > what pressure do you want to be at? As it turns out, super high > > > pressures don't help your density that much and, more importantly, they > > > are worse for your pressure to density ratio which is maximum at the > > > supercritical transition. But let's say 5000psi for some reasonable > > > density. And lets assume an ideal sphere that uses all of the N2 and no > > > payload or mass other than the tank. > > > > > > With Al 6061-T6 you can get 390 m/s, maybe up to 50,000 ft > > > With Maraging Steel 350 (the best strength to weight metal) you get 770 > > > m/s, probably just over 100 kft 1/3rd the way to space > > > With a tank of pure spectra 2000 (the best strength to weight thing I > > > know of) you get 2295 m/s - We made it! Now to make a perfect spherical > > > structure with no binder. > > > But with something that could make a space elevator (~ 10x better than > > > the spectra) you get 4100 m/s - a two stage vehicle and you might make > orbit > > > > > > Now if we used hydrogen at 10000 psi instead of nitrogen, we get a 290s > > > Isp, but at a much lower density it still improves performance and you > > > can get to 9500 m/s - Single stage to orbit! > > > > > > Sorry, I was nerd sniped and thought I should share. All joking aside, > > > cold gas thrusters are useful, but I think Niven was probably just > using > > > a literary Deus Ex Machina when he talked about degenerate matter. > > > > It would take a whole passel of energy to force matter into > > near-degenerate condition. If you then let it expand then the repulsion > > between particles would cause them to gain great velocity. We are > > potentially talking about a good fraction of the speed of light here. > > > > So yes, I think it would work, and it would make a good sci-fi drive. > > But as to how it could be done in practice ... > > > > > > Note that in an ordinary gas the particles do not repel each other, so > > as the gas expands and the distance between the particles increases they > > do not gain energy. As the particles are on average moving away from > > each other, when they bounce off each other their speed drops a little, > > and this causes cooling. > > > > Expanding from the near-degenerate state, where increasing the > > seperation of the particles releases mind-boggling amounts of energy, > > the increased energy would completely overwhelm the cooling effect. > > > > Suddenly releasing the compression would result in a release of energy > > which would be more powerful than a similarly-sized atom bomb going off. > > Depending on exact conditions, it could be considerably more powerful. > > > > -- Peter Fairbrother > > > > > > Lloyd > > > > > > On Wed, Feb 18, 2015 at 11:35 AM, Galejs, Robert - 1007 - MITLL > > > <galejs@xxxxxxxxxx <mailto:galejs@xxxxxxxxxx>> wrote: > > > > > > I know this is way off-topic, but it has always had me wondering > and > > > it seems like Arocket has the appropriate knowledge base to address > > > this (or, at least wildly speculate)...____ > > > > > > __ __ > > > > > > In some of Larry Niven's sci-fi stories, he imagines rocket > > > thrusters (between the ground and orbit) based on super-compressed > > > air (supposedly "nearly degenerate matter"). Would such thrusters > > > theoretically work, or are there some thermodynamic (or other > > > physics) limitations that come into play?____ > > > > > > __ __ > > > > > > Thanks,____ > > > > > > __ __ > > > > > > Robert____ > > > > > > > > -- Christopher Shay <https://sites.google.com/site/chrisshay1/> (407) 566-8256 (321) 443-1451 - Mobile chrisshay1@xxxxxxxxx * "The era we are living in today is a dream come true." * *--Walt Disney*