| | #1 (permalink) |
| Thinking Join Date: Jul 2005
Posts: 294
![]() ![]() | What kind of launch vehicle for manned Spaceflight? Assuming that the support for manned spaceflight continues in the face of the ongoing expense and problems that plague the Space Shuttle; -what kind of launch vehicle would you use in place of the shuttle? -would you use expendable boosters or try for a totally reuseable system? -what would you like to see as the ultimate near term goal for manned spaceflight for the replacement vehicle? How would you justify the investment in a new launch vehicle to the average taxpayer? Damocles |
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| | #2 (permalink) |
| Creating Join Date: Sep 2002 Location: Southern California, USA
Posts: 1,042
![]() ![]() ![]() ![]() ![]() ![]() | Re: What kind of launch vehicle for manned Spaceflight? Before you build a modality you ask what it will be asked to accomplish. Do you want a heavy lifter for colonizing the moon? Ring a Saturn V with eight Space Scuttle solid fuel boosters - use once and toss. That will give you a payload of about 700 tonnes compared to the Space Scuttle's 15 tonnes and be much cheaper per gram boosted. The Space Scuttle costs $30/gram to low Earth orbit. Look up the price of gold. A single Space Scuttle launch coasts $800 million. The payload is never the important part. NASA is buying publicity. http://www.mazepath.com/uncleal/nasa3.htm Do you want to boost smaller payloads? We already have used car lots filled with working possiblities - NASA, ESA, China, Russia... civilian and military. There is no need for a "next generation" booster because we already have every imaginable niche overpopulated with solutions stored as inventory. The needs are to kill off the obscenely expensive and useless Space Scuttle, kill off obscenely expensive and useless International Space Station Freedom FUBAR Space Hole One, and kill off most of obscenely expensive and useless NASA. Before you farm, before you even till the soil, you ask a smple question: What can I plant that will be worth having in large quantities? That will be salable at large profit? The real world answer is inevitably "drugs," and that is the NASA product. Now you proceed onward from there. (The Space Scuttle was originally spec'd at 30 tonnes maximum payload. Added safety hardware upgrades and engineering peformance downgrades have cut that about in half.) The moon is an exceptional platform for physically huge antennas (deep radio to x-ray astronomy) and wonderful launch platform for massive space endeavors (no air resistance and 1/6 gravity, plus its angular mometum of orbit). There isn't much else in local space that is worth visiting for any reason except curiosity - and that is best accomplished with robotics.
__________________ Uncle Al http://www.mazepath.com/uncleal/ (Toxic URL! Unsafe for children and most mammals) http://www.mazepath.com/uncleal/lajos.htm#a2 |
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| | #3 (permalink) |
| Thinking Join Date: Jul 2005
Posts: 294
![]() ![]() | Re: What kind of launch vehicle for manned Spaceflight? Greetings sir. http://hypography.com/forums/showthread.php?p=51387#post51387 I love satire! Couple of things; 1. Nobody sane trusts a thirty year old rocket. 2. The jigs for building new Saturn boosters don't exist any more. 3. We need to get off this rock and spread out. Too many eggs in one basket. 4. Robotics makes sense, since you can scale from micro- to macro- by using incrementalism. After all, as you said, we don't have the lift in the inventory to put heavy stuff into orbit. The big problem is selling the program to a schmuck(me). I know that the future resource base for humans is space. That the true measure of the standard of living for your average schmuck is the amount of energy he uses per volume over time. The more energy you have the richer you are. I want to get to a place where we can tap energy cheaply. The moon is the first place where a micro-machine step up technology might get us the resources to build a truly massive energy base for exploitation. Consider; 1. Fossil fuel extraction fell below demand last year and will continue to fall as China and India look for more oil to power their new industries. 2. Planet based energy production leads to heat pollution(global warming is just a small part of this problem) and heavy metal poisoning of the aquifer. We need alternatives. 3. Most of the solutions that are in the niche lifter category; are barely beyond V-2 engineering, and are throwaway launchers. They are also ozone destroying;(like the SRBs of the "scuttle" for example) so most of the solutions are really non-starters for the massive numbers of launchings that any true any space program.(even for the X-ray astronomy antennae.). Brute forcing that to the moon requires either a hundred 100 kg loftings of manufactory robots which will build the antennae in about ten years, or a hundred 100,000 kilogram "manned" missions, and then you still have to build the antennae with locally available lunar resources(still takes ten years and you have to build a self sustaining base.). You might as well make, it, the seedling mission go, whole hog and go the whole O'Neill route. Damocles Last edited by damocles; 08-15-2005 at 10:27 AM. |
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| | #4 (permalink) |
| Understanding Join Date: May 2005
Posts: 383
![]() ![]() ![]() ![]() | Re: What kind of launch vehicle for manned Spaceflight? I'm not sure where you get 100,000 kilos nor 100 launches from. 100 tonnes is more than enough for a bootstrapping colony. Your low estimate of ten tonnes is too low, though. You need electricity, so solar cells and power storage go up first, along with a bit of basic tough gear which transmits a radio locator beacon, a basic 360 view camera, and perhaps some water. Next you take up cutting tools that work without moving parts, such as plasma cutters, and use these to concentrate the power and melt the regolith for a suitable distance around the base to provide for a landing pad that won't raise dust. You also take up some basic shielding materials which can be used to shelter under in the event of a solar flare, etc. which can later be used to line and seal an underground base area. This is started to be excavated at this stage on a small scale. The walls would be glassy regolith at first, then, once the regolith was breached, it would be solid rock. The walls are unlikely to need extra support at 1/6th earth gravity, unless dusty. Next we need something to create oxygen - the oxygen from regolith idea may help a lot with this, but it will still need storage. In the absence of wind, however, a puncture-proof balloon might be useful for this. If enough power can be concentrated, fused rock as concrete, or even metal casting might be available. Another idea might be to have a system similar to the direct metal sintering 3d printers available now, only using regolith instead of metal powders. This would allow almost anything to be made to the right size and shape from native materials. I've got to go out now, so I'll post more latter. |
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| | #5 (permalink) | |
| Thinking Join Date: Jul 2005
Posts: 294
![]() ![]() | Re: What kind of launch vehicle for manned Spaceflight? Quote:
I don't think we are starting from the same base assumption. You are thinking of building a manned base through fully functioning teleoperated robots. I, instead, am operating from the assumption that you send simple machines to survey, and then to separate out and harvest raw resources, then build a crude solar power station, then build a crude smelter, then build a first stage fabricator, then climb the materials fabrication technology tree until you can custom design on Earth the device/tool you need and either cast or grow it in a liunar fabricator via teleoperation. Once you can design to demand and fabricate at will in situ, then you can think about sending men. You start building the habitat at that point. The point is that the first teleoperated robots needn't be that big with current technology to seed a site for exploitation. Your estimate that 100 tons is sufficient for a manned bootstrap colony is unrealistic. A human uses at least a kilogram of food, another kilogram of water and at least five kilograms of air. Recycling is not 100% efficient. There will be liquid and gaseous waste that will leak from the containment. Also recycling will be massive per human as it will be biomass based for greatest resilience and least susceptibility to mechanical casualties. I doubt that 100 tons will land more than the basics for a 10 man crew for a month. building an x-ray astronomy antennae(the example) will require closer to 10,000 tons of supplies to sustain a crew of 100 men for the two to five years to try and rush the job to completion. As a side note how many tons of supply does the ISS require to sustain its crew in a year? http://www.comspacewatch.com/news/viewnews.html?id=997 Each Progress resupply mission carries abvout 2400 hours(100 days) consumables for the ISS. A Progress rocket carries abou 2 tons(2000 kilograms) of supplies four times a year to the ISS or about 8-10 tons for a crew of three for one year in near earth orbit. A useful lunar base(thirty personnel) would require about 100 tons of supply for sustainment. That does not include subsequent base expansion, the components for brute force building a lunar site based recycling capacity etc. just to dump an Earth launched system of shelters for a five man mission for three months well exceeds the 100 tons postulated. It makes more sense to build the infrastructure first robotically in situ, then send the men. My estimates may be off by one factor, but given that we have never done this before, I am betting my estimates are not pessimistics when it comes to our robotics capabilities and may be wildly optiimistic when it comes to our manned capability! Damocles Last edited by damocles; 08-06-2005 at 07:35 PM. | |
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| | #6 (permalink) | |
| Understanding Join Date: May 2005
Posts: 383
![]() ![]() ![]() ![]() | Re: What kind of launch vehicle for manned Spaceflight? Actually, I was working on the assumption that we use a robotic front line to start the building, then move a couple of people up there once things were nearly ready. As the base expands, more people could go up. NASA seems to be very confident that large amounts of breathable air can be obtained from the regolith, so little extra would be needed once a system was in place. Pressure tanks might be heavy and hard to move up there, but they are much lighter if they are almost empty (or full of vacuum, as it were!) Quote:
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| | #7 (permalink) | |
| Creating Join Date: Sep 2002 Location: Southern California, USA
Posts: 1,042
![]() ![]() ![]() ![]() ![]() ![]() | Re: What kind of launch vehicle for manned Spaceflight? Quote:
Three augmented Saturn V launches is a permanent lunar base : 1) Boost a modified NR-1 nuclear sub and miscellaneous supplies into Earth orbit (400 tonnes fully loaded with a crew of 12. That leaves you 300 more tonnes booster capacity for more supplies or for an emergency trip home vehicle). 2) Boost a year or more of supplies, consummables, spare parts, and construction equipment. Cover your butt. Doing it over costs more than doing it right the first time. 3) Boost the thruster packages for lunar insertion and landing. Assemble and get on with it. 4) The whole thing costs less than the Space Scuttle program to date. There is no reason to use a large /_\v orbit to ship the hardware. Have it economially arrive. Fast boost human meat through the van Allen radiation belts as with Apollo. Proceed from there. No Space Scuttle. The human meat ships in cheap disposable capsules. If you add solar panels the nuclear reactor only works half time. (Batteries? waste of mass and high on maintenance.) That suggests one or two central power bases and lots of peripheral settlements. Long distance electrical wiring is easy - drop uninsulated conductors onto the surface. Use a berm of local dirt to keep them separated. Cheap, easy, proven, and off-the-shelf. We now have a permanent lunar base staffed with 10-100 folks in 1-10 buried huts. What will we do with it all? (Studies!) Oh yeah... blackwater. Dig a big deep hole at the edge of the base and pump sewage in it when things are cold during the 14-day night. Garbage goes into the same hole. The surface area of the moon is 37.8 million km^2 or Africa plus Australia, or all of North America plus Europe. Lots of room.
__________________ Uncle Al http://www.mazepath.com/uncleal/ (Toxic URL! Unsafe for children and most mammals) http://www.mazepath.com/uncleal/lajos.htm#a2 | |
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| | #8 (permalink) | ||||
| Creating Join Date: May 2005 Location: Silver Spring, MD, USA
Posts: 4,511
![]() ![]() ![]() ![]() ![]() ![]() ![]() ![]() ![]() ![]() ![]() | Quote:
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That wasn’t really me writing – perhaps it was the channeled spirit of a turn-of-the-90 or 00s, inside-the-beltway economist. Seriously, the average taxpayer may be fine with buying cheap American flags from the PRC, but might have some misgivings about an imported national space program. Not to mention the big and small US aerospace companies, and the US Congress.The real me is a politically and economically oblivious techie who isn’t happy unless I’ve redesigned at least one perfectly adequate system each day before breakfast. That person would like the US’s next manned spaceflight system to embody the most avant-garde engineering available (which can be taken essentially verbatim from the books and essays of he late Robert Forward), something like the following:
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| | #9 (permalink) |
| Explaining Join Date: Dec 2004
Posts: 583
![]() ![]() | Re: What kind of launch vehicle for manned Spaceflight? space elevator. direct link to space without explosives. mag-lev all the way to space. the system can be powered from space by solar power, if there is enough excess, that power can be pumped into the local power grid.
__________________ don't call me skinny! i'm just ... <<< ... aerodynamic!its in my initials, an anagram.. seriously! |
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| | #10 (permalink) |
| Thinking Join Date: Jul 2005
Posts: 294
![]() ![]() | Re: What kind of launch vehicle for manned Spaceflight? Replies to various from Damocles. First, nobody has solved the heat dumping problem for a large fission reactor in space. We use water chiller convection cooling for nuclear reactors on Earth. Despite this I believe a heat radiator system using a circulation fluid could work in space. It is heavy. Second, We CANNOT build Saturn 5's anymore. We would have to build new heavy lift boosters from SSTS components(Space Shuttle engines, SRBs, fuel tanks etc). That would be as expensive, as designing new, so take your pick. Either discreditted 1970's systems or try for something different? Third. has anyone considered what the SIZE of a LINAC launcher powerful enough to put useful payload(10 tons) into LEO would be? The atmospheric shockwave is a tertiary consideration. The heat loading that you have to deal with and the electrical requirements are insane by our current realistic technical capabilities. Fourth, we cannot use atomics to launch(treaty) anything. Fifth, do we have the materials to build a beanstalk? I would suggest that if we had to scrap plans for the SCRAMJET for the moment because we coiuldn't solve the engine cooling problems that we would have problems with 1, 3, and 5. Option 2 is doable if you have the political will. Option 4(ORION) is prohibited, though a ground based MASER induced pulsed detonation rocket might be a treaty dodge? Damocles |
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