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It's easy to miss how clever the Apollo mission architecture was. The moon is not so far away in terms of distance but it is very far away in terms of Δv because, not least, you have to land propulsively because there is no atmosphere to slow you down. Trips to some near-Earth asteroids are easier than the lunar surface, Mars and Venus aren't that much harder because in any of those cases the Moon's gravity can be helpful. Werner von Braun's early plans to go to the moon https://www.scribd.com/doc/118710867/Collier-s-Magazine-Man-... involved multiple launches, space stations, etc. The recognition that you could get there and back with 7 "stages" * Saturn V 1 * Saturn V 2 * Saturn V 3 * Service Module * Command Module * Bottom half of Lunar Module * Top half of Lunar Module was the key to realizing Kennedy's dream to do it in a decade. |
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You gotta get off Earth no matter where you go in space. It's almost free to come home from LEO, you get a huge amount of free velocity change returning from the moon. (At the cost of rejecting the heat) In the rocket equation https://en.wikipedia.org/wiki/Tsiolkovsky_rocket_equation the required mass ratio is an exponential function of the velocity change so adding another 2.5 km/sec for this and another 2.5 km/sec for that you are making the mission much more difficult. It's bad enough that it takes two stages to get to LEO comfortably but going beyond that adds cost and complexity pretty quick, for instance the large number of Starship launches required to get a Moon mission into the right orbit. I like to think about what interstellar travellers would do if they wanted to land on the Earth on the assumption that they are accustomed to life in deep space and have spent 1,000 to 10,000 years "living off the land" off comets and rouge planets and are used to a lifestyle like cutting up a planet like Pluto and building a number of small ringworlds powered by D-D fusion. I'd conjecture that despite having advanced technology they would still find the "reverse space shuttle" problem where you land with a full load of fuel and then take off from the ground to be difficult. It's not like they are going to haul a space shuttle along with them and would probably find it non-trivial to 3-d print one from plans that old. My take is that it would probably take them a decade to figure it out and that they might well come up with an alternative answer like https://en.wikipedia.org/wiki/Skyhook_(structure) which depends on in-space infrastructure that they'd be experience with although it could work together with an air-breathing aircraft which would be something new for them. |
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Everything is on the small order of magnitude when compared with getting into Earth orbit. As the quote goes, "Once you get to earth orbit, you're halfway to anywhere in the solar system."
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That might be Heinlein's most annoying quote ever and boy does it have competition. It is very expensive to change orbits. If you had two space stations like the ISS with ascending nodes 180 degrees from each other it would be about as expensive to transit between them as it is to launch a rocket from the Earth to begin with. See https://caseyhandmer.wordpress.com/2019/10/02/there-are-no-g... You've got the advantage in space that you can use electric rockets with a high specific impulse. Back in the 1950s folks like von Braun imagined that manned space flight might use electric rockets but after they discovered the Van Allen belts they discovered this is much too slow to make it through the magnetosphere. |
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The space race likely necessitated NASA to show some improvement frequently. Otherwise the Soviet Union would have filled the large gaps between infrequent launches with their incremental successes.
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I would argue plenty of lander designs (including LM) were tailless and landed on their butts! That should be easier than the balancing act of standing on the tail.
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So far the cost is at infinity dollars per ton, give or take a few billion. The focus on launches is because a single launch failure has the ability to make all the rest go to waste. |
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It's important to remember that Apollo was one of Kennedy's signature political projects at the time he was assassinated, which was an important factor in its political viability.
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It had considerable impact on why it had so much leeway compared to pretty much any later work by NASA. When Apollo ended, "space race" ended for USA and it decided to stop on laurels. |
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You're probably right. I wasn't alive nor in the US during that period, so can only infer from what I've seen and read, but I would wager that even the staunchest opponents of the US space program back then couldn't have helped but feel pride of what their country accomplished in such a short time. And even if the majority opposed it, I still think that overall the amount of supporters then would've been greater than the amount of people who support it today. We're living in a time of ignorance and public disinterest in science that Carl Sagan predicted in the '90s[1], which didn't exist in the '60s. That spirit of optimism was partly what enabled such grand scientific projects, and I think most Americans were deeply moved by the words of JFK in that historic 1962 speech[2]. [1]: https://www.goodreads.com/quotes/632474-i-have-a-foreboding-... |
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During the Apollo era NASA was receiving nearly 5% of the federal budget. https://upload.wikimedia.org/wikipedia/commons/thumb/0/09/NA... Apollo was a development and technical marvel. I don't think I would necessarily consider it done in an "optimal way" except for optimizing for time at great expense. Artemis certainly isn't fiscally optimal either, mostly driven by a bunch of stipulations in their budget placed there by senators from states where all of these Shuttle-derived parts are built. |
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SpaceX is a business controlled by a single man that is really interested in making humanity multi-planetary by building a self-sustaining base on Mars.
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I think space expansion business might be more appropriate verbiage. "Exploitation" has connotations of man-vs-man colonialism, which I don't think apply in the case of outer space. |
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I feel exploitation is apt: * Whoever gets to Mars (and the Moon for that matter) first in a permanent fashion gets to write all the rules. Full stop. It's also why the US really does not want China achieving a Moon presence first. * Starlink is competing (and winning) against all the incumbent ISPs for being pieces of shit one way or another, especially incumbent satellite ISPs like Hughesnet who are their immediate competitors. It's all man vs. man colonialism in the end. Besides, "to exploit" something means to make productive use of something: https://www.merriam-webster.com/dictionary/exploit |
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Yes, the article lists a few reasons, none of them convincing. Specifically: > You have to get the propellant into space. This is going to take a large number of flights (~15) at a pace that has not been done before for a vehicle of that size (a launch every six days) SpaceX has done 2 Falcon 9 launches in 1 day, and they would have done 3 if the third one had not have been scrubbed [1]. I really don't think that launching Starship is going to be any different, especially as it was specifically designed for reuse, unlike Falcon 9. > You need to launch at pace because otherwise the propellant will boil off, which is another issue - you need to shade or insulate the propellant for a much longer period of time in much harsher conditions First part is same argument as above. Second part (shading) - again, I don't see why it is harder than other hard things. Just add more insulation. Possibly do some passive or active cooling. > There is no gravity: whereas on earth the propellant separates relatively cleanly into liquid and gas this isn't the case in space Very similar problem to how you feed liquid propellant into a rocket engine when it relights in zero gravity. You use a small ullage thruster for this. [1] https://news.satnews.com/2024/03/31/spacex-enjoys-two-out-of... |
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> There is no gravity: whereas on earth the propellant separates relatively cleanly into liquid and gas this isn't the case in space can you use a plunger, instead of a pump? more like a syringe? |
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Yeah, a 9 meter diameter one, which adds mass and volume and complexity and detracts from the payload. Instead what they do is use thrust to accelerate the whole vehicle a little, which presses all the liquid into one end of its tank where it can be pumped out. Instead of carrying special settling thrusters, they originally planned to use ullage gas for this but it's not clear that can work. deeper discussion with math: https://forum.nasaspaceflight.com/index.php?topic=60124.60 |
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The advanced technologies you're describing are part of Artemis. The other part is a huge pork barrel jobs project for the SLS workforce across the country, in as many states as possible.
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Hmm... so it's really a half-mission to Mars with the Moon as stand-in? That makes a lot more sense. It's still sub-optimal but not as bad as it looks at first glance. |
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> Artificial gravity is easily generated via rotation or thrust. https://space.stackexchange.com/questions/1308/why-are-there... Sure, "easily". > It will be far easier to get materials into space from the moon than from the much deeper gravity well of earth. No it won't, for a very, very simple reason: Every single kilogram of stuff you launch from the moon, has to be launched FIRST from exactly that "deeper gravity well" here on Earth. Including btw. the fuel required to launch it. Because the Moon is shockingly devoid of any steelworks, factories, fuel refineries, Astronaut training facilities, food processing plants or any of the other myriad sources of stuff required in space. So yeah, launching something from 1/6th of Earths gravity is easier. However, all this does, is add another launch to the equation. > How do you see us developing the technology for humans to leave the solar system if we never develop the technology to visit the moon? For the same reason why we developed radio transmission, without first inventing super-sonic carrier pidgeons. Technology does not only advance incrementially. Ever so often, a radically new technology emerges, that is leaps and bounds better than existing systems, and often wasn't developed from these systems either. And btw. Rocket Engines are just one such technology as it happens. Before them, the strongest way to propel something through the air, were propellers, a technology which we since improved by alot, but is still incapable (and never will be capable to) put things into space. So no, doing what we have done before is not a reqirement for finding a much better way to do it. > Also, you don't need to "cheat physics" to explore space. Where exactly did I assume that? But you do need to cheat our current understanding of physics for FTL travel. |
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>https://space.stackexchange.com/questions/1308/why-are-there... > Sure, "easily". The top post of the link is talking about building a ship with a diameter of 200m. In reality you would just need a tether and counterweight. So yes, as far as new space technology goes, "easily." > No it won't, for a very, very simple reason: > Every single kilogram of stuff you launch from the moon, has to be launched FIRST... etc That is the entire point of building out the moon. Sure the investment is difficult, but the longterm return makes it worthwhile. Your argument seems similar to saying "why would we build a steel foundry, when we will need steel to build it in the first place." > How do you see us developing the technology for humans to leave the solar system if we never develop the technology to visit the moon? etc.. The technological difficulty with going to the moon is way more than just rocketry. There's life support systems, shielding, navigation, long term space habitation etc... There are literally hundred if not thousands of technologies that will need to be refined over time, and manned moon missions will go a long way to advancing them. > But you do need to cheat our current understanding of physics for FTL travel. My point was that you do not need ftl to travel through space. |
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> We covered more ground in a lunar rover in a week than any of our mars rovers covered in a year. And this counters my argument...how exactly? Even forgetting the fact that scientific progress isn't measured in "kilometers driven" (just count the number of experiments that Perseverance carries, and compare the amounts of data produced(, there is no technical reason a robot cannot drive as far as a vehicle carrying humans. In fact it's the opposite: One of the most important restrictions regarding the LRVs driving distance wasn't technological in nature, it was due to the the fact it had to carry humans: https://en.wikipedia.org/wiki/Lunar_Roving_Vehicle#Usage An operational constraint on the use of the LRV was that the astronauts must be able to walk back to the LM if the LRV were to fail at any time during the EVA (called the "Walkback Limit"). Thus, the traverses were limited in the distance they could go at the start and at any time later in the EVA. And even though they relaxed the constraints later on, the fact still remains: As soon as you have a human in the mix, things become more cumbersome, way more expensive, slower, less risks can be taken, and if things go wrong, the results can suddenly involve dead people instead of just trashed equipment. |
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> I have low expectations for a robotic field geologist built on a NASA budget. And yet they have put one on Mars. https://en.wikipedia.org/wiki/Perseverance_(rover)#Instrumen... Thing is: Building something that can autonomously navigate the many many variables of city traffic without killing people in the process, is a whole different problem space than building something that can stick a scientific instrument into the ground in an empty rock-desert. > the humans surveyed more ground Again: Scientific progress is not measured in "kilometers driven". And what "surveying" were they doing exactly? How many experiments did they perform during these runs? How many Terabytes of Data did these excursions produce per kilometer driven? I don't know the number tbh. but I am willing to bet that the Mars rovers did better. ALOT better. But okay, if you want to measure distance, lets: Perseverance (which is still active btw.) covered 25.113 km so far. The Ingenuity drone (which perseverance carried), covered a total of 17.242 km. So that's a grand total (so far, again, Perseverance is still active) of 42.355 km. The longest LRV drive was LVR-3 on Apollo 17: 35.89 km. And, let's be clear: That is the total of all its excursions, not a single drive. So yeah, sorry, but the robots have also out-distanced humans already. Comfortably so. > Ultimately we're going to colonize space No, we're not, until such time as we figure out how to leave the solar system and travel to other Earth-like planets. That seems unfair and unsatisfying, I know, but there is simply no way around the facts: other than Earth, every single place in the solar system that doesn't just outright kill humans the moment they leave the spacecraft (and quite a few would kill people instantly even before that), is less hospitable than Earth would be during an ice age, or after a nuclear war. |
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I think if we follow your logic exactly, and make mathematically optimal decisions in every instance, leaving no space for the human spirit - we're robots anyway and may as well go to space!
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If you're paying double for it, why are you getting the SLS for that price? Which, as the article painfully shows, INCREASES risk. By a lot.
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Ouch, that's gotta hurt.. I'm not saying I disagree, but I do wonder if a project is going "right" only when it starts to hit excruciatingly long shifts and burns workforce like coals - especially if it is expected to safely carry humans to the Moon. I think it's more likely a sign of doing something that wasn't planned and budgeted properly (which may certainly be because it simply had never been done before - so it will often correlate with innovative projects). If you worry about your workforce being motivated, transparently tying compensation to company success does wonders.